PSLV R/B, 44234 (Decayed)
Orbit data source: Space-Track
PSLV R/B, 44234 was space debris in LEO originally from a launch on Wed, 22 May 2019 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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44234 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
VSSC/LPSC
Mission
Decayed spacecraft
Bus & Motor
PS-4, Unknown motor
Mass
920 kg wet, 920 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + Cyl + 2 Nozzle, 1.5 m
Radar Cross Section
3.727 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 PSLV R/B
1 44234U 19028B 26055.53635881 .05723466 37575-5 50095-3 0 9991
2 44234 36.9986 0.2289 0004202 263.9067 96.1241 16.38137855378156Epoch: 2026-02-24T12:52Z
TLE epoch observation values (Epoch: 2026-02-24T12:52:21.401Z)
Latitude
-0.00003°
Longitude
12.72521°
Altitude
170.13 km
Speed
7.806 km/s
True Right ascension
00h 00m 54s
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
21:30:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.591 km
Perigee altitude
171.084 km
Semi-major axis
6,551.975 km
Eccentricity
0.00042
Inclination
36.9986°
RAAN
0.2289°
Arg. of periapsis
263.9067°
True anomaly
96.17197°
Mean anomaly
96.1241°
Eccentric anomaly
96.14804°
Mean motion
4.09246 °/min
Orbital period
87.97 mins
BSTAR
0.00050095
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Other satellites on launch #28 in the year 2019 (2019-05-22 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.PSLV R/B Visibility
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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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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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