GSLV R/B, 62851
Orbit data source: Space-Track
GSLV R/B, 62851 is space debris in HEO originally from a launch on Wed, 29 Jan 2025 UTC launched from the Sirharikota (SRI). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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62851 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 GSLV R/B
1 62851U 25020B 25246.64750118 .00089892 15719-5 33038-2 0 9995
2 62851 21.1100 359.7282 7250805 328.4424 3.6536 2.35913096 4891
Epoch: 2025-09-03T15:32Z
TLE epoch observation values (Epoch: 2025-09-03T15:32:24.101Z)
Latitude
-0.00007°
Longitude
143.61317°
Altitude
584.662 km
Speed
9.887 km/s
True Right ascension
23h 58m 56s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
20:16:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,748.809 km
Perigee altitude
176.108 km
Semi-major axis
23,840.595 km
Eccentricity
0.72508
Inclination
21.11°
RAAN
359.7282°
Arg. of periapsis
328.4424°
True anomaly
31.84984°
Mean anomaly
3.6536°
Eccentric anomaly
12.99652°
Mean motion
0.58961 °/min
Orbital period
610.57 mins
BSTAR
0.0033038
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Other satellites on launch #20 in the year 2025 (2025-01-29 UTC)
GSLV R/B Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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547 mins | 2025-09-07 11:06:49.646Z | 210.069° SW | 2025-09-07 11:22:49.646Z | 142.85° SSE | 35.615° | 2025-09-07 20:13:49.646Z | 149.3° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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