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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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Non-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: 17 hours ago
TLE from 17 hours ago
0 NVS-02
1 62850U 25020A 26154.61908606 .00000887 00000-0 59413-3 0 9992
2 62850 20.7241 264.1601 7347929 140.2358 307.6735 2.17968267 10687Epoch: 2026-06-03T14:51Z
TLE epoch observation values (Epoch: 2026-06-03T14:51:29.035Z)
Latitude
0.0002°
Longitude
149.17299°
Altitude
20,203.066 km
Speed
3.759 km/s
True Right ascension
17h 36m 28s
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
18:07:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,219.847 km
Perigee altitude
286.921 km
Semi-major axis
25,131.521 km
Eccentricity
0.73479
Inclination
20.7241°
RAAN
264.1601°
Arg. of periapsis
140.2358°
True anomaly
219.86598°
Mean anomaly
307.6735°
Eccentric anomaly
265.69192°
Mean motion
0.54477 °/min
Orbital period
660.83 mins
BSTAR
0.00059413
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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. |
|---|---|---|---|---|---|---|---|
| 18 mins | 2026-06-04 14:03:17.211Z | 252.481° W | 2026-06-04 14:17:17.211Z | 212.371° SW | 19.337° | 2026-06-04 14:21:17.211Z | 170.047° S |
| 341 mins | 2026-06-05 02:36:17.211Z | 195.515° SSW | 2026-06-05 06:07:17.211Z | 203.206° SW | 22.64° | 2026-06-05 08:17:17.211Z | 222.739° SW |
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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