PSLV R/B, 44104 (Decayed)
Orbit data source: Space-Track
PSLV R/B, 44104 was space debris in LEO originally from a launch on Mon, 01 Apr 2019 UTC via a PSLV-QL launch vehicle 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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44104 intel report (Beta)
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PSLV R/B radio frequencies
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO SAC/Banga
Mission
Decayed Civil Technology
Bus & Motor
PS-4 OP, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Box, 0.1 m
Radar Cross Section
0.075 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 PSLV R/B
1 44104U 19018AC 24182.30226727 .75017961 27951-5 13042-3 0 9996
2 44104 97.3313 295.7289 0014430 174.9294 243.0071 16.64608738295003Epoch: 2024-06-30T07:15Z
TLE epoch observation values (Epoch: 2024-06-30T07:15:15.892Z)
Latitude
57.16302°
Longitude
-103.37182°
Altitude
115.088 km
Speed
7.84 km/s
True Right ascension
18h 57m 11s
True Declination
56° 59' 26"
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
01:29:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
107.265 km
Perigee altitude
88.575 km
Semi-major axis
6,476.057 km
Eccentricity
0.00144
Inclination
97.3313°
RAAN
295.7289°
Arg. of periapsis
174.9294°
True anomaly
242.85988°
Mean anomaly
243.0071°
Eccentric anomaly
242.93348°
Mean motion
4.16464 °/min
Orbital period
86.44 mins
BSTAR
0.00013042
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Other satellites on launch #18 in the year 2019 (2019-04-01 UTC)
PSLV 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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