SCOUT A R/B, 1953
Orbit data source: Space-Track
SCOUT A R/B, 1953 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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1953 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SCOUT A R/B
1 1953U 66005B 26095.21734204 .00000191 00000-0 18639-3 0 9991
2 1953 90.1515 351.5330 0228681 41.1026 320.7110 13.65064111992925Epoch: 2026-04-05T05:12Z
TLE epoch observation values (Epoch: 2026-04-05T05:12:58.352Z)
Latitude
-0.00007°
Longitude
79.76393°
Altitude
890.994 km
Speed
7.471 km/s
True Right ascension
23h 26m 07s
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
00:28:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,183.423 km
Perigee altitude
845.318 km
Semi-major axis
7,392.507 km
Eccentricity
0.02287
Inclination
90.1515°
RAAN
351.533°
Arg. of periapsis
41.1026°
True anomaly
319.01436°
Mean anomaly
320.711°
Eccentric anomaly
319.86645°
Mean motion
3.41472 °/min
Orbital period
105.43 mins
BSTAR
0.00018639
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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 R/B 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-04-06 04:39:14.709Z | 18.093° NNE | 2026-04-06 04:45:14.709Z | 93.148° ESE | 33.433° | 2026-04-06 04:51:14.709Z | 156.267° SSE |
| 9 mins | 2026-04-06 06:26:14.709Z | 331.306° NNW | 2026-04-06 06:30:14.709Z | 279.271° WNW | 27.028° | 2026-04-06 06:35:14.709Z | 226.325° WSW |
| 8 mins | 2026-04-06 16:32:14.709Z | 129.085° SE | 2026-04-06 16:35:14.709Z | 84.292° E | 27.446° | 2026-04-06 16:40:14.709Z | 18.229° NNE |
| 8 mins | 2026-04-06 18:17:14.709Z | 224.299° SW | 2026-04-06 18:21:14.709Z | 284.67° WNW | 25.594° | 2026-04-06 18:25:14.709Z | 333.658° NNW |
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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