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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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: 11 hours ago
TLE from 11 hours ago
0 GARAI-A
1 62635U 25009AC 26107.84056886 .00004882 00000-0 22117-3 0 9997
2 62635 97.4012 188.8104 0003311 154.7471 205.3927 15.21320891 69616Epoch: 2026-04-17T20:10Z
TLE epoch observation values (Epoch: 2026-04-17T20:10:25.149Z)
Latitude
-0.00005°
Longitude
40.23764°
Altitude
507.006 km
Speed
7.609 km/s
True Right ascension
12h 35m 14s
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
13:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.096 km
Perigee altitude
496.542 km
Semi-major axis
6,876.956 km
Eccentricity
0.00033
Inclination
97.4012°
RAAN
188.8104°
Arg. of periapsis
154.7471°
True anomaly
205.37644°
Mean anomaly
205.3927°
Eccentric anomaly
205.38457°
Mean motion
3.80582 °/min
Orbital period
94.59 mins
BSTAR
0.00022117
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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 | 2026-04-18 17:17:03.563Z | 61.387° ENE | 2026-04-18 17:19:03.563Z | 97.895° ESE | 15.142° | 2026-04-18 17:21:03.563Z | 131.591° SE |
| 4 mins | 2026-04-18 18:51:03.563Z | 330.776° NNW | 2026-04-18 18:53:03.563Z | 275.482° WNW | 25.585° | 2026-04-18 18:55:03.563Z | 234.391° WSW |
| 5 mins | 2026-04-19 05:28:03.563Z | 172.163° S | 2026-04-19 05:30:03.563Z | 286.791° WNW | 44.651° | 2026-04-19 05:33:03.563Z | 345.776° 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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