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 Commercial Imaging
Bus & Motor
DRISHTI, Unknown motor
Mass
190 kg wet, 190 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.8 m
Radar Cross Section
2.180 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 DRISHTI
1 69010U 26100AG 26265.93799881 .00001680 00000-0 79173-4 0 9996
2 69010 97.3902 161.9594 0006704 56.6195 303.5681 15.20847253 21660Epoch: 2026-09-22T22:30Z
TLE epoch observation values (Epoch: 2026-09-22T22:30:43.097Z)
Latitude
-0.00003°
Longitude
-177.51647°
Altitude
503.826 km
Speed
7.614 km/s
True Right ascension
10h 47m 50s
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
08:35:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.859 km
Perigee altitude
495.636 km
Semi-major axis
6,878.385 km
Eccentricity
0.00067
Inclination
97.3902°
RAAN
161.9594°
Arg. of periapsis
56.6195°
True anomaly
303.50406°
Mean anomaly
303.5681°
Eccentric anomaly
303.53608°
Mean motion
3.80464 °/min
Orbital period
94.62 mins
BSTAR
0.000079173
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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 | 2026-09-23 17:36:14.971Z | 202.259° SSW | 2026-09-23 17:38:14.971Z | 274.479° WNW | 43.667° | 2026-09-23 17:41:14.971Z | 333.505° NNW |
| 4 mins | 2026-09-24 06:40:14.971Z | 330.502° NNW | 2026-09-24 06:42:14.971Z | 275.207° WNW | 28.922° | 2026-09-24 06:44:14.971Z | 234.351° WSW |
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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