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Near Reentry Satellite
The table shows the satellites that will reenter Earth's atmosphere over the next 1000 days. Usually they are old satellites at low altitude, the remains of rockets or parts of satellites that collided. The ISS (International Space Station) appears in the list because it suffers a strong drag on the atmosphere, which requires constant corrections for altitude.
Satellite Launch Norad Incl.
degrees
Apogee
Km
Perigee
Km
Period
min
Options
CZ-2F R/B
Reentry: (YMD) 2021-11-1
202149327U4116013287Tracking | Reentry
ELECTRON R/B
Reentry: (YMD) 2021-11-15
202149053U3719415988Tracking | Reentry
ELECTRON KICK STAGE R/B
Reentry: (YMD) 2021-11-23
202149473U4226815289Tracking | Reentry
SL-4 R/B
Reentry: (YMD) 2021-11-26
202149500U5214914687Tracking | Reentry
STARLINK-2277
Reentry: (YMD) 2021-11-29
202148006U5314413887Tracking | Reentry
STARLINK-1875
Reentry: (YMD) 2021-11-29
202047160U5317416688Tracking | Reentry
STARLINK-2262
Reentry: (YMD) 2021-11-29
202148001U5314914487Tracking | Reentry
FALCON 9 DEB
Reentry: (YMD) 2021-11-30
202149468U5321817188Tracking | Reentry
FALCON 9 DEB
Reentry: (YMD) 2021-11-30
202149461U5323217589Tracking | Reentry
ELECTRON R/B
Reentry: (YMD) 2021-12-1
202149472U4227018089Tracking | Reentry
FALCON 9 DEB
Reentry: (YMD) 2021-12-1
202149463U5322617589Tracking | Reentry
FALCON 9 DEB
Reentry: (YMD) 2021-12-1
202149462U5323317789Tracking | Reentry
STARLINK-3123
Reentry: (YMD) 2021-12-1
202149429U5322617488Tracking | Reentry
STARLINK-2203
Reentry: (YMD) 2021-12-4
202147417U9731931791Tracking | Reentry
STARLINK-2206
Reentry: (YMD) 2021-12-4
202147420U9731931791Tracking | Reentry
STARLINK-2207
Reentry: (YMD) 2021-12-4
202147421U9733233091Tracking | Reentry
STARLINK-2199
Reentry: (YMD) 2021-12-5
202147413U9731731491Tracking | Reentry
STARLINK-2200
Reentry: (YMD) 2021-12-5
202147414U9731731591Tracking | Reentry
STARLINK-2205
Reentry: (YMD) 2021-12-5
202147419U9732232091Tracking | Reentry
STARLINK-2079
Reentry: (YMD) 2021-12-5
202147364U5331131091Tracking | Reentry
STARLINK-1757
Reentry: (YMD) 2021-12-5
202046339U5329328890Tracking | Reentry
SL-4 R/B
Reentry: (YMD) 2021-12-11
202149128U9623322489Tracking | Reentry
AZTECHSAT-1
Reentry: (YMD) 2021-12-11
199845261U5227926890Tracking | Reentry
STARLINK-2287
Reentry: (YMD) 2021-12-13
202148035U5332431891Tracking | Reentry
STARLINK-2259
Reentry: (YMD) 2021-12-13
202148007U5332232091Tracking | Reentry
STARLINK-2311
Reentry: (YMD) 2021-12-13
202147987U5332232091Tracking | Reentry
STARLINK-2302
Reentry: (YMD) 2021-12-13
202148024U5332232091Tracking | Reentry
STARLINK-2289
Reentry: (YMD) 2021-12-13
202147983U5332232091Tracking | Reentry
STARLINK-2261
Reentry: (YMD) 2021-12-13
202148004U5332232091Tracking | Reentry
STARLINK-2281
Reentry: (YMD) 2021-12-14
202148015U5332431891Tracking | Reentry
SPACEBEE-9
Reentry: (YMD) 2021-12-16
201944370U4531529791Tracking | Reentry
STARLINK-1097
Reentry: (YMD) 2021-12-16
202044916U5330330091Tracking | Reentry
LEMUR-2-BAXTER-OLIVER
Reentry: (YMD) 2021-12-20
199846925U5229528790Tracking | Reentry
NARSSCUBE-1
Reentry: (YMD) 2021-12-23
199844792U5229328390Tracking | Reentry
2020-063G
Reentry: (YMD) 2021-12-27
202046395U5024824389Tracking | Reentry
CHEFSAT
Reentry: (YMD) 2021-12-28
201743044U5232531791Tracking | Reentry
STARLINK-1023
Reentry: (YMD) 2021-12-29
201944728U5330729991Tracking | Reentry
LEMUR-2-DJARA
Reentry: (YMD) 2022-01-4
199846926U5232632191Tracking | Reentry
STARLINK-2297
Reentry: (YMD) 2022-01-6
202148032U5334533691Tracking | Reentry
1998-067RU
Reentry: (YMD) 2022-01-7
199846924U5232431691Tracking | Reentry
STARLINK-1943
Reentry: (YMD) 2022-01-20
202046795U5331130891Tracking | Reentry
STARLINK-1204
Reentry: (YMD) 2022-01-25
202045203U5330129991Tracking | Reentry
STARLINK-1367
Reentry: (YMD) 2022-01-26
202045539U5334533991Tracking | Reentry
KRAKSAT
Reentry: (YMD) 2022-01-30
199844427U5231831091Tracking | Reentry
STARLINK-1674
Reentry: (YMD) 2022-02-13
202046555U5330029991Tracking | Reentry
1998-067RC
Reentry: (YMD) 2022-02-18
199845259U5234633591Tracking | Reentry
STARLINK-1853
Reentry: (YMD) 2022-03-2
202047140U5333531991Tracking | Reentry
QARMAN
Reentry: (YMD) 2022-03-2
199845263U5234533591Tracking | Reentry
FALCON 9 DEB
Reentry: (YMD) 2022-03-8
202046090U5333432691Tracking | Reentry
STARLINK-1051
Reentry: (YMD) 2022-03-10
201944756U5330129791Tracking | Reentry
STARLINK-2318
Reentry: (YMD) 2022-03-12
202148025U5332632291Tracking | Reentry
STARLINK-2366
Reentry: (YMD) 2022-03-21
202147906U5334133991Tracking | Reentry
AEOLUS
Reentry: (YMD) 2022-04-21
201843600U9731730591Tracking | Reentry
SL-3 R/B
Reentry: (YMD) 2022-05-3
198516111U9732931891Tracking | Reentry
STARLINK-1501
Reentry: (YMD) 2022-05-7
202045763U5334033991Tracking | Reentry
FALCON 9 DEB
Reentry: (YMD) 2022-05-20
202046087U5334933891Tracking | Reentry
Satellites Orbital Parameters

The table above shows the main parameters and information available for this satellite.

Satellite: This column shows the name of the object in orbit. In some cases the official name ends with the words R/B, meaning that it is a piece or any stage from some rocket booster.

Norad: North American Aerospace Defense Command, the Air Defence Command of the United States, responsible for the catalogue of objects in orbit. The number indicates the record of the satellite in the Norad archives.

Inclination: Angle formed between the orbit of the satellite and terrestrial line of the equator. Satellites with inclination of 0 degrees follow the equator line and are called equatorial orbit satellites. When the inclination is 90 degrees its orbit crosses the terrestrial poles and are called polar orbiting satellites. When the inclination is less or equal latitude of the place of observation, the satellite be seen directly if conditions permit.

Apogee: Maximum distance that the object is far from the center of the Earth.

Perigee: Highest approchement between the object and the center of the Earth. The figures shown already discounting the radius of the Earth, 6378 Km. One Perigee value equal to the value of Apogee indicates a circular orbit satellite.

Period: Value in minutes that a satellite takes to complete one orbit of perigee to perigee. Satellites in polar orbit, positioned at 800 km in altitude will take approximately 102 minutes to complete one revolution. The International Space Station, 350 km above the surface, completes its orbit in 90 minutes.

The lower the altitude of a satellite, more speed he needs to keep in orbit and not re-enters the atmosphere.

Geostationary satellites have a period of approximately 1436 minutes with inclination of 0 degrees (equatorial orbit). Because this is the same time it takes Earth to complete one turn on its axis, geostationary satellites appear static on the same geographic point. To this happens the satellite should be positioned about 36 thousand kilometers in altitude.

Note and Frequency: Filled with additional information where possible. The frequencies shown, when provided, are those captured by enthusiasts or informed by the official organizations of disclosure.

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