USA 97, 22915
Orbit data source: Space-Track
USA 97, 22915 is an American payload satellite in GEO that was launched on Sun, 28 Nov 1993 UTC via an ATLAS II 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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22915 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
MM/Valley Forge
Mission
Non-operational Defense Communications
Bus & Motor
DSCS III, AOCS
Mass
~1,232 kg wet, ~900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Poly + 2 Pan, 4.8 m
Radar Cross Section
8.439 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 USA 97
1 22915U 93074A 26258.86997917 .00000006 00000-0 00000-0 0 9997
2 22915 13.8762 14.7980 0004796 18.5265 334.2278 0.98533104 25795Epoch: 2026-09-15T20:52Z
TLE epoch observation values (Epoch: 2026-09-15T20:52:46.200Z)
Latitude
-1.74354°
Longitude
59.69995°
Altitude
36,262.483 km
Speed
3.058 km/s
True Right ascension
00h 30m 53s
True Declination
-1° 44' 30"
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
04:01:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,302.593 km
Perigee altitude
36,261.673 km
Semi-major axis
42,660.27 km
Eccentricity
0.00048
Inclination
13.8762°
RAAN
14.798°
Arg. of periapsis
18.5265°
True anomaly
334.20389°
Mean anomaly
334.2278°
Eccentric anomaly
334.21585°
Mean motion
0.24632 °/min
Orbital period
1,461.49 mins
BSTAR
0
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Other satellites on launch #74 in the year 1993 (1993-11-28 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.USA 97 Visibility
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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. |
|---|---|---|---|---|---|---|---|
| USA 97 is likely not visible in the next few days. |
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22915 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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