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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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: 19 hours ago
TLE from 19 hours ago
0 EOS-8
1 60454U 24147A 26319.01399595 .00056215 00000-0 65079-3 0 9998
2 60454 37.3790 173.1757 0003231 346.4430 13.6252 15.60791186126556Epoch: 2026-11-15T00:20Z
TLE epoch observation values (Epoch: 2026-11-15T00:20:09.250Z)
Latitude
0.00002°
Longitude
114.02666°
Altitude
382.393 km
Speed
7.684 km/s
True Right ascension
11h 32m 42s
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
16:22:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
390.474 km
Perigee altitude
386.101 km
Semi-major axis
6,766.424 km
Eccentricity
0.00032
Inclination
37.379°
RAAN
173.1757°
Arg. of periapsis
346.443°
True anomaly
13.63393°
Mean anomaly
13.6252°
Eccentric anomaly
13.62956°
Mean motion
3.89946 °/min
Orbital period
92.32 mins
BSTAR
0.00065079
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-15 20:38:06.487Z | 259.108° W | 2026-11-15 20:41:06.487Z | 182.31° SSW | 53.357° | 2026-11-15 20:44:06.487Z | 104.038° ESE |
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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