OBJECT A, 100080
Orbit data source: Space-Track
OBJECT A, 100080 is an Indian satellite in LEO that was launched on Sat, 18 Jul 2026 UTC launched from the Sirharikota (SRI). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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100080 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
GRAHAA
Mission
Operational spacecraft
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
BOX, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 OBJECT A
1 A0080U 26164A 26219.50718637 .00004009 00000-0 10804-3 0 9993
2 A0080 59.9264 225.7099 0013621 323.8573 36.1592 15.39896694 3125Epoch: 2026-08-07T12:10Z
TLE epoch observation values (Epoch: 2026-08-07T12:10:20.902Z)
Latitude
-0.00002°
Longitude
87.0909°
Altitude
440.516 km
Speed
7.653 km/s
True Right ascension
15h 02m 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
01:03:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.918 km
Perigee altitude
436.328 km
Semi-major axis
6,823.76 km
Eccentricity
0.00136
Inclination
59.9264°
RAAN
225.7099°
Arg. of periapsis
323.8573°
True anomaly
36.25142°
Mean anomaly
36.1592°
Eccentric anomaly
36.2053°
Mean motion
3.85042 °/min
Orbital period
93.5 mins
BSTAR
0.00010804
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Other satellites on launch #164 in the year 2026 (2026-07-18 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.OBJECT A 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-09 01:42:32.503Z | 184.608° SSW | 2026-08-09 01:45:32.503Z | 121.153° SE | 26.931° | 2026-08-09 01:48:32.503Z | 59.68° ENE |
| 4 mins | 2026-08-09 03:20:32.503Z | 281.387° WNW | 2026-08-09 03:22:32.503Z | 328.881° NNW | 20.153° | 2026-08-09 03:24:32.503Z | 7.509° NNE |
| 4 mins | 2026-08-09 09:53:32.503Z | 354.401° N | 2026-08-09 09:54:32.503Z | 24.319° NE | 31.546° | 2026-08-09 09:57:32.503Z | 112.056° ESE |
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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