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, 0.5 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 TSAT-1A
1 59442U 24066A 26306.84282154 .00010359 00000-0 29834-3 0 9990
2 59442 45.6145 83.1642 0009893 187.6188 172.4558 15.36003309143081Epoch: 2026-11-02T20:13Z
TLE epoch observation values (Epoch: 2026-11-02T20:13:39.781Z)
Latitude
-0.00006°
Longitude
97.63436°
Altitude
464.713 km
Speed
7.632 km/s
True Right ascension
05h 32m 39s
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
09:22:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.218 km
Perigee altitude
452.689 km
Semi-major axis
6,837.59 km
Eccentricity
0.00099
Inclination
45.6145°
RAAN
83.1642°
Arg. of periapsis
187.6188°
True anomaly
172.47067°
Mean anomaly
172.4558°
Eccentric anomaly
172.46323°
Mean motion
3.83874 °/min
Orbital period
93.78 mins
BSTAR
0.00029834
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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 | 2026-11-03 13:39:21.432Z | 264.878° W | 2026-11-03 13:42:21.432Z | 356.623° N | 54.006° | 2026-11-03 13:45:21.432Z | 58.706° ENE |
| 4 mins | 2026-11-03 15:19:21.432Z | 317.79° NNW | 2026-11-03 15:20:21.432Z | 345.148° N | 30.663° | 2026-11-03 15:23:21.432Z | 58.441° ENE |
| 5 mins | 2026-11-03 16:57:21.432Z | 309.927° NW | 2026-11-03 16:59:21.432Z | 15.918° NNE | 50.966° | 2026-11-03 17:02:21.432Z | 92.949° ESE |
| 5 mins | 2026-11-03 18:35:21.432Z | 271.556° WNW | 2026-11-03 18:37:21.432Z | 220.056° SW | 35.277° | 2026-11-03 18:40:21.432Z | 150.362° SSE |
| 5 mins | 2026-11-04 11:26:21.432Z | 190.899° SSW | 2026-11-04 11:28:21.432Z | 145.722° SSE | 26.691° | 2026-11-04 11:31:21.432Z | 85.836° E |
| 5 mins | 2026-11-04 13:04:21.432Z | 263.34° W | 2026-11-04 13:06:21.432Z | 330.252° NNW | 62.181° | 2026-11-04 13:09:21.432Z | 58.905° ENE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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