GSLV R/B, 56082 (Decayed)
Orbit data source: Space-Track
GSLV R/B, 56082 was space debris in LEO originally from an Indian launch on Sun, 26 Mar 2023 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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56082 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Decayed spacecraft
Bus & Motor
C25, CE-20
Mass
4,400 kg wet, 4,400 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 6.8 m
Radar Cross Section
48.836 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 GSLV R/B
1 56082U 23043AN 24166.54356647 .24880644 -14000-5 14634-3 0 9990
2 56082 87.3709 340.3933 0012142 257.4446 216.5646 16.54439776 69393Epoch: 2024-06-14T13:02Z
TLE epoch observation values (Epoch: 2024-06-14T13:02:44.143Z)
Latitude
66.03019°
Longitude
55.49532°
Altitude
145.574 km
Speed
7.821 km/s
True Right ascension
10h 17m 59s
True Declination
65° 53' 25"
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
11:48:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
132.207 km
Perigee altitude
116.417 km
Semi-major axis
6,502.449 km
Eccentricity
0.00121
Inclination
87.3709°
RAAN
340.3933°
Arg. of periapsis
257.4446°
True anomaly
216.48181°
Mean anomaly
216.5646°
Eccentric anomaly
216.5232°
Mean motion
4.13931 °/min
Orbital period
86.97 mins
BSTAR
0.00014634
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Other satellites on launch #43 in the year 2023 (2023-03-26 UTC)
GSLV R/B Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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