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: 3 days ago
TLE from 3 days ago
0 EOS-8
1 60454U 24147A 26077.71432808 .00022505 00000-0 46183-3 0 9991
2 60454 37.3798 269.3677 0004142 304.0821 55.9549 15.45244051 89068Epoch: 2026-03-18T17:08Z
TLE epoch observation values (Epoch: 2026-03-18T17:08:37.946Z)
Latitude
-0.00003°
Longitude
-164.06458°
Altitude
428.235 km
Speed
7.658 km/s
True Right ascension
17h 57m 28s
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
05:44:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
436.38 km
Perigee altitude
430.737 km
Semi-major axis
6,811.695 km
Eccentricity
0.00041
Inclination
37.3798°
RAAN
269.3677°
Arg. of periapsis
304.0821°
True anomaly
55.99424°
Mean anomaly
55.9549°
Eccentric anomaly
55.97457°
Mean motion
3.86065 °/min
Orbital period
93.25 mins
BSTAR
0.00046183
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-22 14:24:03.710Z | 190.191° SSW | 2026-03-22 14:26:03.710Z | 152.845° SSE | 15.231° | 2026-03-22 14:28:03.710Z | 116.114° SE |
| 4 mins | 2026-03-22 16:02:03.710Z | 226.102° WSW | 2026-03-22 16:04:03.710Z | 150.429° SSE | 33.088° | 2026-03-22 16:06:03.710Z | 102.552° ESE |
| 4 mins | 2026-03-22 17:40:03.710Z | 250.119° W | 2026-03-22 17:42:03.710Z | 156.43° SSE | 37.375° | 2026-03-22 17:44:03.710Z | 111.237° ESE |
| 4 mins | 2026-03-22 19:18:03.710Z | 239.943° WSW | 2026-03-22 19:19:03.710Z | 215.068° SW | 23.601° | 2026-03-22 19:22:03.710Z | 144.35° 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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