SCOUT A DEB, 2226
Orbit data source: Space-Track
SCOUT A DEB, 2226 is space debris in LEO originally from a launch on Wed, 22 Dec 1965 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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2226 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 SCOUT A DEB
1 02226U 65109D 25258.67282509 .00000109 00000-0 11938-3 0 9999
2 02226 89.0692 332.9945 0249620 118.0235 244.6409 13.51176064916612Epoch: 2025-09-15T16:08Z
TLE epoch observation values (Epoch: 2025-09-15T16:08:52.087Z)
Latitude
-0.0001°
Longitude
95.90336°
Altitude
1,154.243 km
Speed
7.235 km/s
True Right ascension
22h 11m 58s
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
10:40:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,250.777 km
Perigee altitude
879.187 km
Semi-major axis
7,443.119 km
Eccentricity
0.02496
Inclination
89.0692°
RAAN
332.9945°
Arg. of periapsis
118.0235°
True anomaly
242.09104°
Mean anomaly
244.6409°
Eccentric anomaly
243.36248°
Mean motion
3.37995 °/min
Orbital period
106.51 mins
BSTAR
0.00011938
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Other satellites on launch #109 in the year 1965 (1965-12-22 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.SCOUT A DEB 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-19 03:49:41.843Z | 111.67° ESE | 2025-09-19 03:53:41.843Z | 70.212° E | 16.863° | 2025-09-19 03:56:41.843Z | 38.78° NE |
| 10 mins | 2025-09-19 05:34:41.843Z | 192.879° SSW | 2025-09-19 05:39:41.843Z | 293.722° NW | 41.696° | 2025-09-19 05:44:41.843Z | 351.64° N |
| 9 mins | 2025-09-19 16:43:41.843Z | 16.448° NNE | 2025-09-19 16:47:41.843Z | 95.366° ESE | 39.456° | 2025-09-19 16:52:41.843Z | 164.351° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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