SCOUT A DEB, 2140
Orbit data source: Space-Track
SCOUT A DEB, 2140 is space debris in LEO originally from a launch on Fri, 28 Jan 1966 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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2140 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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SCOUT A DEB
1 02140U 66005C 26038.46098103 .00000285 00000-0 32802-3 0 9997
2 02140 89.9525 51.1084 0315458 199.8208 159.0460 13.48380117940979Epoch: 2026-02-07T11:03Z
TLE epoch observation values (Epoch: 2026-02-07T11:03:48.760Z)
Latitude
0.00002°
Longitude
107.57106°
Altitude
1,301.791 km
Speed
7.098 km/s
True Right ascension
03h 24m 26s
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
09:05:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,310.396 km
Perigee altitude
840.148 km
Semi-major axis
7,453.409 km
Eccentricity
0.03155
Inclination
89.9525°
RAAN
51.1084°
Arg. of periapsis
199.8208°
True anomaly
160.29267°
Mean anomaly
159.046°
Eccentric anomaly
159.67384°
Mean motion
3.37296 °/min
Orbital period
106.73 mins
BSTAR
0.00032802
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Other satellites on launch #5 in the year 1966 (1966-01-28 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.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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-09 11:46:54.598Z | 30.905° NE | 2026-02-09 11:50:54.598Z | 71.975° E | 20.04° | 2026-02-09 11:54:54.598Z | 121.549° SE |
| 9 mins | 2026-02-09 13:33:54.598Z | 346.624° N | 2026-02-09 13:37:54.598Z | 294.955° NW | 36.318° | 2026-02-09 13:42:54.598Z | 209.784° SW |
| 10 mins | 2026-02-09 23:45:54.598Z | 120.434° SE | 2026-02-09 23:49:54.598Z | 81.084° E | 25.905° | 2026-02-09 23:55:54.598Z | 22.669° NE |
| 13 mins | 2026-02-10 01:29:54.598Z | 196.503° SSW | 2026-02-10 01:36:54.598Z | 283.211° WNW | 39.617° | 2026-02-10 01:42:54.598Z | 346.865° 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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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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