GARAI-A, 62635
Orbit data source: Space-Track
GARAI-A, 62635 is a payload satellite owned by Satlantis (ES) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62635 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
OHB-SE
Mission
Operational Commercial Imaging
Bus & Motor
INNOSAT, Unknown motor
Mass
115 kg wet, 115 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 3.0 m
Radar Cross Section
1.305 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 GARAI-A
1 62635U 25009AC 25292.90900179 .00018669 00000-0 82748-3 0 9995
2 62635 97.4227 11.6053 0003905 86.3430 273.8252 15.21655138 42251Epoch: 2025-10-19T21:48Z
TLE epoch observation values (Epoch: 2025-10-19T21:48:57.754Z)
Latitude
-0.00008°
Longitude
15.74576°
Altitude
503.762 km
Speed
7.612 km/s
True Right ascension
00h 46m 25s
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
01:15:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.497 km
Perigee altitude
495.127 km
Semi-major axis
6,875.949 km
Eccentricity
0.00039
Inclination
97.4227°
RAAN
11.6053°
Arg. of periapsis
86.343°
True anomaly
273.78055°
Mean anomaly
273.8252°
Eccentric anomaly
273.80288°
Mean motion
3.80666 °/min
Orbital period
94.57 mins
BSTAR
0.00082748
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.GARAI-A 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 | 2025-10-20 17:20:16.739Z | 56.04° ENE | 2025-10-20 17:22:16.739Z | 91.993° ESE | 16.338° | 2025-10-20 17:24:16.739Z | 129.195° SE |
| 4 mins | 2025-10-20 18:54:16.739Z | 333.378° NNW | 2025-10-20 18:56:16.739Z | 284.436° WNW | 24.476° | 2025-10-20 18:58:16.739Z | 240.064° WSW |
| 5 mins | 2025-10-21 05:31:16.739Z | 176.118° S | 2025-10-21 05:33:16.739Z | 249.066° W | 43.98° | 2025-10-21 05:36:16.739Z | 343.388° N |
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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