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: 6 hours ago
TLE from 6 hours ago
0 TSAT-1A
1 59442U 24066A 25344.54251809 .00018983 00000-0 64309-3 0 9998
2 59442 45.6189 67.8979 0008038 142.4367 217.7089 15.30347183 92821Epoch: 2025-12-10T13:01Z
TLE epoch observation values (Epoch: 2025-12-10T13:01:13.562Z)
Latitude
-0.00007°
Longitude
153.07998°
Altitude
479.203 km
Speed
7.625 km/s
True Right ascension
04h 31m 35s
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
17:00:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.792 km
Perigee altitude
470.773 km
Semi-major axis
6,854.42 km
Eccentricity
0.0008
Inclination
45.6189°
RAAN
67.8979°
Arg. of periapsis
142.4367°
True anomaly
217.65261°
Mean anomaly
217.7089°
Eccentric anomaly
217.68075°
Mean motion
3.82461 °/min
Orbital period
94.13 mins
BSTAR
0.00064309
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-11 07:59:37.407Z | 184.924° SSW | 2025-12-11 08:01:37.407Z | 149.953° SSE | 18.502° | 2025-12-11 08:04:37.407Z | 93.798° ESE |
| 6 mins | 2025-12-11 09:37:37.407Z | 249.704° W | 2025-12-11 09:40:37.407Z | 37.037° NE | 43.125° | 2025-12-11 09:43:37.407Z | 63.26° ENE |
| 4 mins | 2025-12-11 11:17:37.407Z | 308.564° NW | 2025-12-11 11:19:37.407Z | 12.168° NNE | 28.191° | 2025-12-11 11:21:37.407Z | 53.664° ENE |
| 5 mins | 2025-12-11 12:56:37.407Z | 319.736° NNW | 2025-12-11 12:58:37.407Z | 33.229° NE | 32.281° | 2025-12-11 13:01:37.407Z | 84.933° E |
| 5 mins | 2025-12-11 14:34:37.407Z | 282.962° WNW | 2025-12-11 14:36:37.407Z | 227.821° WSW | 39.55° | 2025-12-11 14:39:37.407Z | 134.493° SE |
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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