NISAR, 65053
Orbit data source: Space-Track
NISAR, 65053 is an Indian payload satellite in SSO that was launched on Wed, 30 Jul 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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65053 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Operational Civil Radar Imaging
Bus & Motor
I3K, ISRO LAM
Mass
2,393 kg wet, ~2,300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 14.3 m
Radar Cross Section
10.461 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 NISAR
1 65053U 25163A 26208.60430691 -.00000036 00000-0 23095-5 0 9997
2 65053 98.4058 35.6798 0001159 89.4782 270.6540 14.42505010 52213Epoch: 2026-07-27T14:30Z
TLE epoch observation values (Epoch: 2026-07-27T14:30:12.117Z)
Latitude
-0.00006°
Longitude
-127.15618°
Altitude
753.179 km
Speed
7.478 km/s
True Right ascension
02h 22m 43s
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
12:10:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
748.174 km
Perigee altitude
746.522 km
Semi-major axis
7,125.485 km
Eccentricity
0.00012
Inclination
98.4058°
RAAN
35.6798°
Arg. of periapsis
89.4782°
True anomaly
270.64072°
Mean anomaly
270.654°
Eccentric anomaly
270.64736°
Mean motion
3.60846 °/min
Orbital period
99.77 mins
BSTAR
0.0000023095
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Other satellites on launch #163 in the year 2025 (2025-07-30 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.NISAR 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-07-28 01:04:01.002Z | 23.851° NE | 2026-07-28 01:08:01.002Z | 80.162° E | 38.585° | 2026-07-28 01:13:01.002Z | 177.497° S |
| 4 mins | 2026-07-28 02:45:01.002Z | 320.231° NNW | 2026-07-28 02:47:01.002Z | 291.406° WNW | 16.585° | 2026-07-28 02:49:01.002Z | 264.776° W |
| 7 mins | 2026-07-28 12:17:01.002Z | 150.674° SSE | 2026-07-28 12:20:01.002Z | 78.387° E | 42.575° | 2026-07-28 12:24:01.002Z | 354.45° N |
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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