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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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 26076.34133929 -.00000102 00000-0 00000-0 0 9990
2 22796 14.5779 356.2798 0051867 76.9244 118.7122 1.00272046125989Epoch: 2026-03-17T08:11Z
TLE epoch observation values (Epoch: 2026-03-17T08:11:31.714Z)
Latitude
-4.01637°
Longitude
-105.84969°
Altitude
35,892.423 km
Speed
3.067 km/s
True Right ascension
12h 47m 48s
True Declination
-4° 00' 44"
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
19:37:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,006.193 km
Perigee altitude
35,568.792 km
Semi-major axis
42,165.63 km
Eccentricity
0.00519
Inclination
14.5779°
RAAN
356.2798°
Arg. of periapsis
76.9244°
True anomaly
119.23185°
Mean anomaly
118.7122°
Eccentric anomaly
118.97219°
Mean motion
0.25067 °/min
Orbital period
1,436.14 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 | 2026-03-18 14:53:06.133Z | 180.47° SSW | 2026-03-19 01:03:06.133Z | 181.388° SSW | 40.992° | 2026-03-19 14:53:06.133Z | 180.461° SSW |
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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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