AISAT, 40054
Orbit data source: Space-Track
AISAT, 40054 is a payload satellite owned by DLR (DE) in SSO that was launched on Mon, 30 Jun 2014 UTC via a PSLV 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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40054 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
DLR-ISS
Mission
Non-operational Civil Communications
Bus & Motor
CLAVIS, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Truss, 2.0 m
Radar Cross Section
0.040 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 AISAT
1 40054U 14034B 25312.21223779 .00015940 00000-0 11853-2 0 9990
2 40054 98.2505 204.2658 0008233 241.0453 118.9946 15.03052830613944Epoch: 2025-11-08T05:05Z
TLE epoch observation values (Epoch: 2025-11-08T05:05:37.345Z)
Latitude
0.00006°
Longitude
80.21509°
Altitude
563.303 km
Speed
7.578 km/s
True Right ascension
13h 37m 03s
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
16:39:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.223 km
Perigee altitude
548.808 km
Semi-major axis
6,932.653 km
Eccentricity
0.00082
Inclination
98.2505°
RAAN
204.2658°
Arg. of periapsis
241.0453°
True anomaly
119.07708°
Mean anomaly
118.9946°
Eccentric anomaly
119.03584°
Mean motion
3.76005 °/min
Orbital period
95.74 mins
BSTAR
0.0011853
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Other satellites on launch #34 in the year 2014 (2014-06-30 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.AISAT 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-09 05:37:46.463Z | 23.411° NE | 2025-11-09 05:40:46.463Z | 90.711° ESE | 40.621° | 2025-11-09 05:44:46.463Z | 181.789° SSW |
| 5 mins | 2025-11-09 16:23:46.463Z | 121.988° SE | 2025-11-09 16:25:46.463Z | 72.843° E | 29.453° | 2025-11-09 16:28:46.463Z | 10.431° NNE |
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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