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: 12 hours ago
TLE from 12 hours ago
0 NVS-02
1 62850U 25020A 25287.25963123 .00000125 00000-0 32120-3 0 9994
2 62850 21.0986 349.1204 7354192 347.6294 1.4552 2.17521229 5629Epoch: 2025-10-14T06:13Z
TLE epoch observation values (Epoch: 2025-10-14T06:13:52.138Z)
Latitude
-0.00015°
Longitude
-127.39214°
Altitude
340.873 km
Speed
10.139 km/s
True Right ascension
23h 16m 30s
True Declination
0° 00' 01"
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
13:12:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,295.26 km
Perigee altitude
280.279 km
Semi-major axis
25,165.906 km
Eccentricity
0.73542
Inclination
21.0986°
RAAN
349.1204°
Arg. of periapsis
347.6294°
True anomaly
13.96774°
Mean anomaly
1.4552°
Eccentric anomaly
5.47685°
Mean motion
0.54366 °/min
Orbital period
662.18 mins
BSTAR
0.0003212
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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. |
|---|---|---|---|---|---|---|---|
| 151 mins | 2025-10-15 16:07:17.490Z | 271.055° WNW | 2025-10-15 17:22:17.490Z | 256.043° W | 24.471° | 2025-10-15 18:38:17.490Z | 255.817° W |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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