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: 17 hours ago
TLE from 17 hours ago
0 PROVES-ELECTRA
1 69795U 98067YL 26271.57211771 .00061585 00000-0 76547-3 0 9992
2 69795 51.6276 145.1899 0008456 200.2918 159.7740 15.59343246 13725Epoch: 2026-09-28T13:43Z
TLE epoch observation values (Epoch: 2026-09-28T13:43:50.970Z)
Latitude
0.00001°
Longitude
-68.12202°
Altitude
395.67 km
Speed
7.671 km/s
True Right ascension
09h 40m 45s
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
00:05:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
395.792 km
Perigee altitude
384.345 km
Semi-major axis
6,768.206 km
Eccentricity
0.00085
Inclination
51.6276°
RAAN
145.1899°
Arg. of periapsis
200.2918°
True anomaly
159.80747°
Mean anomaly
159.774°
Eccentric anomaly
159.79074°
Mean motion
3.89792 °/min
Orbital period
92.36 mins
BSTAR
0.00076547
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-29 17:34:32.450Z | 189.526° SSW | 2026-09-29 17:36:32.450Z | 149.972° SSE | 24.096° | 2026-09-29 17:39:32.450Z | 78.147° E |
| 4 mins | 2026-09-29 19:11:32.450Z | 279.149° WNW | 2026-09-29 19:13:32.450Z | 350.094° N | 32.097° | 2026-09-29 19:15:32.450Z | 33.495° NE |
| 4 mins | 2026-09-30 00:02:32.450Z | 338.683° N | 2026-09-30 00:04:32.450Z | 46.316° ENE | 30.928° | 2026-09-30 00:06:32.450Z | 91.159° ESE |
| 4 mins | 2026-09-30 01:38:32.450Z | 271.551° WNW | 2026-09-30 01:40:32.450Z | 213.977° SW | 25.608° | 2026-09-30 01:42:32.450Z | 170.375° S |
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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