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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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: 10 hours ago
TLE from 10 hours ago
0 TSAT-1A
1 59442U 24066A 26082.50694028 .00015484 00000-0 47557-3 0 9997
2 59442 45.6166 228.2050 0010736 334.5767 25.4598 15.33609325108611Epoch: 2026-03-23T12:09Z
TLE epoch observation values (Epoch: 2026-03-23T12:09:59.640Z)
Latitude
-0.00005°
Longitude
-135.29151°
Altitude
458.491 km
Speed
7.643 km/s
True Right ascension
15h 12m 49s
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
03:12:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.912 km
Perigee altitude
459.215 km
Semi-major axis
6,844.701 km
Eccentricity
0.00107
Inclination
45.6166°
RAAN
228.205°
Arg. of periapsis
334.5767°
True anomaly
25.51275°
Mean anomaly
25.4598°
Eccentric anomaly
25.48627°
Mean motion
3.83276 °/min
Orbital period
93.93 mins
BSTAR
0.00047557
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-24 11:48:05.388Z | 171.651° S | 2026-03-24 11:50:05.388Z | 130.115° SE | 17.267° | 2026-03-24 11:52:05.388Z | 95.95° ESE |
| 6 mins | 2026-03-24 13:25:05.388Z | 248.089° W | 2026-03-24 13:28:05.388Z | 48.689° ENE | 42.416° | 2026-03-24 13:31:05.388Z | 63.856° ENE |
| 5 mins | 2026-03-24 15:04:05.388Z | 297.16° NW | 2026-03-24 15:06:05.388Z | 346.39° N | 29.019° | 2026-03-24 15:09:05.388Z | 56.524° ENE |
| 5 mins | 2026-03-24 16:43:05.388Z | 312.924° NW | 2026-03-24 16:45:05.388Z | 11.024° NNE | 32.772° | 2026-03-24 16:48:05.388Z | 80.909° E |
| 6 mins | 2026-03-24 18:21:05.388Z | 286.014° WNW | 2026-03-24 18:23:05.388Z | 249.129° W | 38.825° | 2026-03-24 18:27:05.388Z | 129.911° 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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