DRISHTI, 69010
AKA "DRISHTI" on Space-Track | Orbit data source: Space-Track
DRISHTI, 69010 is an Indian payload satellite in SSO that was launched on Sun, 03 May 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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69010 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
GALEYE
Mission
Operational spacecraft
Bus & Motor
DRISHTI, Unknown motor
Mass
190 kg wet, 190 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 DRISHTI
1 69010U 26100AG 26175.19646909 .00002303 00000-0 10857-3 0 9992
2 69010 97.4037 72.8948 0005741 22.9407 337.2084 15.20479329 7878Epoch: 2026-06-24T04:42Z
TLE epoch observation values (Epoch: 2026-06-24T04:42:54.929Z)
Latitude
0.00001°
Longitude
89.80878°
Altitude
503.842 km
Speed
7.614 km/s
True Right ascension
04h 51m 34s
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
08:35:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.308 km
Perigee altitude
497.409 km
Semi-major axis
6,879.496 km
Eccentricity
0.00057
Inclination
97.4037°
RAAN
72.8948°
Arg. of periapsis
22.9407°
True anomaly
337.1829°
Mean anomaly
337.2084°
Eccentric anomaly
337.19565°
Mean motion
3.80372 °/min
Orbital period
94.64 mins
BSTAR
0.00010857
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.DRISHTI 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-25 06:33:53.266Z | 337.407° NNW | 2026-06-25 06:35:53.266Z | 273.13° WNW | 30.577° | 2026-06-25 06:38:53.266Z | 219.419° SW |
| 5 mins | 2026-06-25 17:10:53.266Z | 160.964° S | 2026-06-25 17:12:53.266Z | 129.76° SE | 43.426° | 2026-06-25 17:15:53.266Z | 351.903° N |
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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