POEM 4, 62461 (Decayed)
Orbit data source: Space-Track
POEM 4, 62461 was a payload satellite owned by ISRO (IN) in LEO that was launched on Mon, 30 Dec 2024 UTC via a PSLV launch vehicle from the Sirharikota (SRI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62461 intel report (Beta)
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POEM 4 radio frequencies
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 POEM 4
1 62461U 24253C 25093.60098506 .06123810 12042-4 53849-3 0 9994
2 62461 55.1994 162.5248 0005929 311.9454 141.1615 16.38452900 14905
Epoch: 2025-04-03T14:25Z
TLE epoch observation values (Epoch: 2025-04-03T14:25:25.109Z)
Latitude
55.2296°
Longitude
-150.48786°
Altitude
180.119 km
Speed
7.803 km/s
True Right ascension
17h 12m 09s
True Declination
55° 03' 15"
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
22:16:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
173.731 km
Perigee altitude
165.966 km
Semi-major axis
6,547.985 km
Eccentricity
0.00059
Inclination
55.1994°
RAAN
162.5248°
Arg. of periapsis
311.9454°
True anomaly
141.20408°
Mean anomaly
141.1615°
Eccentric anomaly
141.18279°
Mean motion
4.0962 °/min
Orbital period
87.89 mins
BSTAR
0.00053849
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Other satellites on launch #253 in the year 2024 (2024-12-30 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.POEM 4 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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