EOS-7, 55562 (Decayed)
Orbit data source: Space-Track
EOS-7, 55562 was a payload satellite owned by ISRO (IN) in LEO that was launched on Fri, 10 Feb 2023 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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55562 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO SAC/Banga
Mission
Decayed Civil Imaging
Bus & Motor
IMS-1, Unknown motor
Mass
156 kg wet, ~156 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.540 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 EOS-7
1 55562U 23019A 24363.45300977 .04873498 38898-5 83598-3 0 9991
2 55562 37.1672 46.7039 0002842 101.5126 258.5981 16.31915089106730Epoch: 2024-12-28T10:52Z
TLE epoch observation values (Epoch: 2024-12-28T10:52:20.044Z)
Latitude
-0.00003°
Longitude
146.21686°
Altitude
186.864 km
Speed
7.796 km/s
True Right ascension
03h 06m 48s
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
21:25:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
192.306 km
Perigee altitude
188.572 km
Semi-major axis
6,568.576 km
Eccentricity
0.00028
Inclination
37.1672°
RAAN
46.7039°
Arg. of periapsis
101.5126°
True anomaly
258.56618°
Mean anomaly
258.5981°
Eccentric anomaly
258.58214°
Mean motion
4.07696 °/min
Orbital period
88.3 mins
BSTAR
0.00083598
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Other satellites on launch #19 in the year 2023 (2023-02-10 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-7 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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