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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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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 SCOUT A DEB
1 02226U 65109D 26042.73892782 .00000226 00000-0 27052-3 0 9992
2 02226 89.0643 318.8394 0248981 46.8656 315.3023 13.51240389936749Epoch: 2026-02-11T17:44Z
TLE epoch observation values (Epoch: 2026-02-11T17:44:03.363Z)
Latitude
-0.00004°
Longitude
-88.97534°
Altitude
941.193 km
Speed
7.445 km/s
True Right ascension
21h 15m 21s
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
07:27:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,250.06 km
Perigee altitude
879.432 km
Semi-major axis
7,442.883 km
Eccentricity
0.0249
Inclination
89.0643°
RAAN
318.8394°
Arg. of periapsis
46.8656°
True anomaly
313.2506°
Mean anomaly
315.3023°
Eccentric anomaly
314.28099°
Mean motion
3.38011 °/min
Orbital period
106.51 mins
BSTAR
0.00027052
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-12 05:00:34.334Z | 49.34° ENE | 2026-02-12 05:03:34.334Z | 79.027° E | 14.952° | 2026-02-12 05:06:34.334Z | 107.042° ESE |
| 11 mins | 2026-02-12 06:45:34.334Z | 357.623° N | 2026-02-12 06:50:34.334Z | 259.148° W | 44.567° | 2026-02-12 06:56:34.334Z | 187.872° SSW |
| 11 mins | 2026-02-12 18:42:34.334Z | 177.969° S | 2026-02-12 18:48:34.334Z | 351.772° N | 44.326° | 2026-02-12 18:53:34.334Z | 358.75° N |
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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