EYESAT A, 22825
Orbit data source: Space-Track
EYESAT A, 22825 is a payload satellite owned by Interfer (US) in SSO that was launched on Sun, 26 Sep 1993 UTC via an ARIANE 40 launch vehicle from the French Guiana (FRGUI). 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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22825 intel report (Beta)
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EYESAT A radio frequencies
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Interfer
Mission
Partially operational Commercial Communications
Bus & Motor
MICROSAT, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.135 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 EYESAT A
1 22825U 93061C 25258.11991375 .00000067 00000-0 42577-4 0 9998
2 22825 98.7274 320.1196 0008406 179.7374 180.3814 14.30828500667663Epoch: 2025-09-15T02:52Z
TLE epoch observation values (Epoch: 2025-09-15T02:52:40.547Z)
Latitude
-0.00008°
Longitude
-77.37847°
Altitude
797.917 km
Speed
7.451 km/s
True Right ascension
21h 20m 28s
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
06:51:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
792.13 km
Perigee altitude
780.086 km
Semi-major axis
7,164.245 km
Eccentricity
0.00084
Inclination
98.7274°
RAAN
320.1196°
Arg. of periapsis
179.7374°
True anomaly
180.38076°
Mean anomaly
180.3814°
Eccentric anomaly
180.38108°
Mean motion
3.57921 °/min
Orbital period
100.58 mins
BSTAR
0.000042577
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Other satellites on launch #61 in the year 1993 (1993-09-26 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.EYESAT 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-15 16:52:32.474Z | 20.186° NNE | 2025-09-15 16:57:32.474Z | 107.367° ESE | 42.045° | 2025-09-15 17:01:32.474Z | 181.397° SSW |
| 4 mins | 2025-09-15 18:34:32.474Z | 322.003° NNW | 2025-09-15 18:36:32.474Z | 295.66° NW | 15.409° | 2025-09-15 18:38:32.474Z | 270.279° WNW |
| 9 mins | 2025-09-16 04:10:32.474Z | 165.222° S | 2025-09-16 04:14:32.474Z | 339.061° N | 44.965° | 2025-09-16 04:19:32.474Z | 346.453° N |
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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