EOS-8, 60454
Orbit data source: Space-Track
EOS-8, 60454 is a payload satellite owned by ISRO (IN) in LEO that was launched on Fri, 16 Aug 2024 UTC via an SSLV 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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60454 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO SAC/Banga
Mission
Operational Civil Imaging
Bus & Motor
IMS-1, Unknown motor
Mass
176 kg wet, ~176 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.5 m
Radar Cross Section
0.935 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 EOS-8
1 60454U 24147A 25310.28473544 .00100402 00000-0 22322-2 0 9995
2 60454 37.3825 23.3822 0002422 38.0070 322.0864 15.42443303 68588Epoch: 2025-11-06T06:50Z
TLE epoch observation values (Epoch: 2025-11-06T06:50:01.142Z)
Latitude
-0.00001°
Longitude
-124.86782°
Altitude
436.751 km
Speed
7.653 km/s
True Right ascension
01h 33m 31s
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
15:28:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.446 km
Perigee altitude
440.142 km
Semi-major axis
6,819.931 km
Eccentricity
0.00024
Inclination
37.3825°
RAAN
23.3822°
Arg. of periapsis
38.007°
True anomaly
322.06934°
Mean anomaly
322.0864°
Eccentric anomaly
322.07787°
Mean motion
3.85366 °/min
Orbital period
93.42 mins
BSTAR
0.0022322
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Other satellites on launch #147 in the year 2024 (2024-08-16 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.EOS-8 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-07 09:31:31.592Z | 227.855° WSW | 2025-11-07 09:33:31.592Z | 173.276° S | 32.195° | 2025-11-07 09:36:31.592Z | 98.911° ESE |
| 5 mins | 2025-11-07 11:09:31.592Z | 255.304° W | 2025-11-07 11:11:31.592Z | 203.387° SW | 38.633° | 2025-11-07 11:14:31.592Z | 106.793° ESE |
| 4 mins | 2025-11-07 12:48:31.592Z | 238.261° WSW | 2025-11-07 12:49:31.592Z | 209.951° SW | 26.316° | 2025-11-07 12:52:31.592Z | 138.558° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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