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: 20 hours ago
TLE from 20 hours ago
0 NVS-02
1 62850U 25020A 25337.81693301 .00000956 00000-0 53770-3 0 9996
2 62850 21.0069 330.8855 7347946 20.4476 357.9470 2.17585454 6727Epoch: 2025-12-03T19:36Z
TLE epoch observation values (Epoch: 2025-12-03T19:36:23.012Z)
Latitude
0.00073°
Longitude
-36.1061°
Altitude
504.463 km
Speed
9.999 km/s
True Right ascension
22h 03m 29s
True Declination
0° 00' 03"
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
13:33:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,270.945 km
Perigee altitude
294.683 km
Semi-major axis
25,160.951 km
Eccentricity
0.73479
Inclination
21.0069°
RAAN
330.8855°
Arg. of periapsis
20.4476°
True anomaly
340.52413°
Mean anomaly
357.947°
Eccentric anomaly
352.32243°
Mean motion
0.54382 °/min
Orbital period
661.99 mins
BSTAR
0.0005377
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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. |
|---|---|---|---|---|---|---|---|
| 66 mins | 2025-12-04 15:39:00.543Z | 182.074° SSW | 2025-12-04 15:39:00.543Z | 182.074° SSW | 20.905° | 2025-12-04 16:45:00.543Z | 171.898° S |
| 50 mins | 2025-12-05 04:56:00.543Z | 192.465° SSW | 2025-12-05 05:01:00.543Z | 147.558° SSE | 26.463° | 2025-12-05 05:46:00.543Z | 99.08° ESE |
| 367 mins | 2025-12-05 08:15:00.543Z | 110.018° ESE | 2025-12-05 12:08:00.543Z | 142.183° SSE | 19.71° | 2025-12-05 14:22:00.543Z | 149.418° 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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