ACTS, 22796
Orbit data source: Space-Track
ACTS, 22796 is a payload satellite owned by NASA LeRC (US) in GEO that was launched on Sun, 12 Sep 1993 UTC via an SPACE SHUTTLE launch vehicle from the Air Force Eastern Test Range (AFETR). 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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22796 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
MM/East Windsor
Mission
Non-operational Civil Communications
Bus & Motor
AS4000, Unknown motor
Mass
2,770 kg wet, ~1,488 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Poly + 2 Pan, 1.1 m
Radar Cross Section
4.512 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ACTS
1 22796U 93058B 25350.03620084 -.00000101 00000-0 00000-0 0 9992
2 22796 14.5812 356.9762 0047859 77.4483 277.9753 1.00271314125066Epoch: 2025-12-16T00:52Z
TLE epoch observation values (Epoch: 2025-12-16T00:52:07.752Z)
Latitude
-1.28781°
Longitude
-105.95142°
Altitude
35,759.422 km
Speed
3.077 km/s
True Right ascension
23h 28m 01s
True Declination
-1° 17' 11"
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
08:36:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,989.5 km
Perigee altitude
35,585.897 km
Semi-major axis
42,165.835 km
Eccentricity
0.00479
Inclination
14.5812°
RAAN
356.9762°
Arg. of periapsis
77.4483°
True anomaly
277.43174°
Mean anomaly
277.9753°
Eccentric anomaly
277.70356°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #58 in the year 1993 (1993-09-12 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.ACTS 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-12-17 09:51:51.389Z | 178.116° S | 2025-12-18 07:05:51.389Z | 180.654° SSW | 41.001° | 2025-12-18 09:51:51.389Z | 178.122° S |
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22796 neighbors
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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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