TSAT-1A, 59442
Orbit data source: Space-Track
TSAT-1A, 59442 is a payload satellite owned by TASL (IN) in LEO that was launched on Sun, 07 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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59442 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
URUGUS S.A.
Mission
Operational Commercial Imaging
Bus & Motor
NEWSAT V, Unknown motor
Mass
~42 kg wet, ~38 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 TSAT-1A
1 59442U 24066A 26037.27981345 .00023437 00000-0 74581-3 0 9996
2 59442 45.6165 114.4034 0007933 88.6853 271.4950 15.32242882101670Epoch: 2026-02-06T06:42Z
TLE epoch observation values (Epoch: 2026-02-06T06:42:55.882Z)
Latitude
-0.00001°
Longitude
-122.74941°
Altitude
469.052 km
Speed
7.633 km/s
True Right ascension
07h 37m 36s
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
17:43:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.064 km
Perigee altitude
465.198 km
Semi-major axis
6,848.768 km
Eccentricity
0.00079
Inclination
45.6165°
RAAN
114.4034°
Arg. of periapsis
88.6853°
True anomaly
271.40412°
Mean anomaly
271.495°
Eccentric anomaly
271.44956°
Mean motion
3.82935 °/min
Orbital period
94.01 mins
BSTAR
0.00074581
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Other satellites on launch #66 in the year 2024 (2024-04-07 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.TSAT-1A 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-07 07:56:46.115Z | 216.573° SW | 2026-02-07 07:59:46.115Z | 143.408° SSE | 34.287° | 2026-02-07 08:02:46.115Z | 76.931° E |
| 5 mins | 2026-02-07 09:35:46.115Z | 276.27° WNW | 2026-02-07 09:37:46.115Z | 324.578° NNW | 35.023° | 2026-02-07 09:40:46.115Z | 54.383° ENE |
| 5 mins | 2026-02-07 11:14:46.115Z | 307.109° NW | 2026-02-07 11:16:46.115Z | 354.06° N | 27.856° | 2026-02-07 11:19:46.115Z | 64.172° ENE |
| 5 mins | 2026-02-07 12:53:46.115Z | 304.655° NW | 2026-02-07 12:55:46.115Z | 16.796° NNE | 42.054° | 2026-02-07 12:58:46.115Z | 102.303° ESE |
| 4 mins | 2026-02-07 14:32:46.115Z | 249.963° W | 2026-02-07 14:33:46.115Z | 224.652° SW | 23.142° | 2026-02-07 14:36:46.115Z | 162.76° S |
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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