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: 12 hours ago
TLE from 12 hours ago
0 AISAT
1 40054U 14034B 25310.01529836 .00013776 00000-0 10276-2 0 9992
2 40054 98.2520 201.9260 0007948 249.8479 110.1889 15.02971308613613Epoch: 2025-11-06T00:22Z
TLE epoch observation values (Epoch: 2025-11-06T00:22:01.778Z)
Latitude
-0.00008°
Longitude
150.93892°
Altitude
562.689 km
Speed
7.579 km/s
True Right ascension
13h 27m 42s
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
08:01:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
560.277 km
Perigee altitude
549.256 km
Semi-major axis
6,932.903 km
Eccentricity
0.00079
Inclination
98.252°
RAAN
201.926°
Arg. of periapsis
249.8479°
True anomaly
110.27435°
Mean anomaly
110.1889°
Eccentric anomaly
110.23163°
Mean motion
3.75985 °/min
Orbital period
95.75 mins
BSTAR
0.0010276
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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 | 2025-11-06 16:28:05.694Z | 142.46° SSE | 2025-11-06 16:32:05.694Z | 60.809° ENE | 33.206° | 2025-11-06 16:35:05.694Z | 4.316° NNE |
| 6 mins | 2025-11-07 05:42:05.694Z | 20.96° NNE | 2025-11-07 05:45:05.694Z | 119.24° SE | 42.785° | 2025-11-07 05:48:05.694Z | 184.137° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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