NVS-02, 62850
Orbit data source: Space-Track
NVS-02, 62850 is a payload satellite owned by ISRO (IN) in HEO that was launched on Wed, 29 Jan 2025 UTC via a GSLV MK II 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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62850 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Partially operational Civil Navigation
Bus & Motor
I2K, ISRO LAM
Mass
2,232 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
8.526 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 NVS-02
1 62850U 25020A 26028.41433295 .00001209 00000-0 71243-3 0 9991
2 62850 20.8828 310.6438 7348252 56.6576 353.0613 2.17646153 7937Epoch: 2026-01-28T09:56Z
TLE epoch observation values (Epoch: 2026-01-28T09:56:38.366Z)
Latitude
0.00062°
Longitude
33.89032°
Altitude
1,872.258 km
Speed
8.987 km/s
True Right ascension
20h 42m 55s
True Declination
0° 00' 02"
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
07:19:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,263.624 km
Perigee altitude
292.676 km
Semi-major axis
25,156.287 km
Eccentricity
0.73483
Inclination
20.8828°
RAAN
310.6438°
Arg. of periapsis
56.6576°
True anomaly
302.54067°
Mean anomaly
353.0613°
Eccentric anomaly
335.80777°
Mean motion
0.54397 °/min
Orbital period
661.8 mins
BSTAR
0.00071243
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Other satellites on launch #20 in the year 2025 (2025-01-29 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.NVS-02 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. |
|---|---|---|---|---|---|---|---|
| 514 mins | 2026-01-30 06:35:29.016Z | 241.58° WSW | 2026-01-30 07:08:29.016Z | 186.53° SSW | 29.206° | 2026-01-30 15:09:29.016Z | 213.442° SW |
| 69 mins | 2026-01-31 04:33:29.016Z | 224.163° SW | 2026-01-31 04:44:29.016Z | 174.602° S | 28.872° | 2026-01-31 05:42:29.016Z | 139.246° SSE |
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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