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, 4.8 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 25254.61586327 .00001504 00000-0 73996-3 0 9993
2 62850 21.1288 0.9514 7358994 326.2832 3.7956 2.17438768 4915Epoch: 2025-09-11T14:46Z
TLE epoch observation values (Epoch: 2025-09-11T14:46:50.586Z)
Latitude
0.00001°
Longitude
148.3696°
Altitude
759.306 km
Speed
9.79 km/s
True Right ascension
00h 03m 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
19:13:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,318.398 km
Perigee altitude
269.876 km
Semi-major axis
25,172.274 km
Eccentricity
0.7359
Inclination
21.1288°
RAAN
0.9514°
Arg. of periapsis
326.2832°
True anomaly
34.91368°
Mean anomaly
3.7956°
Eccentric anomaly
13.98593°
Mean motion
0.54345 °/min
Orbital period
662.43 mins
BSTAR
0.00073996
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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. |
|---|---|---|---|---|---|---|---|
| 598 mins | 2025-09-14 09:06:51.227Z | 178.352° S | 2025-09-14 16:31:51.227Z | 135.133° SSE | 32.4° | 2025-09-14 19:04:51.227Z | 141.227° SSE |
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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