PROVES-ELECTRA, 69795
Orbit data source: Space-Track
PROVES-ELECTRA, 69795 is an American payload satellite in LEO that was delivered to the ISS. 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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69795 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
UCSC
Mission
Operational spacecraft
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX, 0.086 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 PROVES-ELECTRA
1 69795U 98067YL 26317.27311368 .00168375 00000-0 14074-2 0 9994
2 69795 51.6260 274.0992 0008541 68.6589 291.5318 15.68919611 20874Epoch: 2026-11-13T06:33Z
TLE epoch observation values (Epoch: 2026-11-13T06:33:17.021Z)
Latitude
-0.0001°
Longitude
123.38358°
Altitude
360.627 km
Speed
7.695 km/s
True Right ascension
18h 16m 23s
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
15:51:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
368.261 km
Perigee altitude
356.747 km
Semi-major axis
6,740.641 km
Eccentricity
0.00085
Inclination
51.626°
RAAN
274.0992°
Arg. of periapsis
68.6589°
True anomaly
291.44072°
Mean anomaly
291.5318°
Eccentric anomaly
291.48626°
Mean motion
3.92185 °/min
Orbital period
91.79 mins
BSTAR
0.0014074
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Other satellites on launch #67 in the year 1998 (1998-11-20 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.PROVES-ELECTRA 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-13 23:32:16.071Z | 196.103° SSW | 2026-11-13 23:34:16.071Z | 148.198° SSE | 29.459° | 2026-11-13 23:36:16.071Z | 82.823° E |
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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