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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Edit Public Description
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 SCOUT A R/B
1 01953U 66005B 25323.80268066 .00000155 00000-0 14840-3 0 9997
2 01953 90.1465 349.4467 0229372 85.6621 277.0709 13.65025557974310Epoch: 2025-11-19T19:15Z
TLE epoch observation values (Epoch: 2025-11-19T19:15:51.609Z)
Latitude
0.0001°
Longitude
1.41248°
Altitude
1,003.423 km
Speed
7.358 km/s
True Right ascension
23h 17m 47s
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
06:10:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,184.076 km
Perigee altitude
844.943 km
Semi-major axis
7,392.647 km
Eccentricity
0.02294
Inclination
90.1465°
RAAN
349.4467°
Arg. of periapsis
85.6621°
True anomaly
274.45415°
Mean anomaly
277.0709°
Eccentric anomaly
275.76334°
Mean motion
3.41463 °/min
Orbital period
105.43 mins
BSTAR
0.0001484
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-20 13:26:28.407Z | 24.181° NE | 2025-11-20 13:31:28.407Z | 95.05° ESE | 29.664° | 2025-11-20 13:36:28.407Z | 151.009° SSE |
| 8 mins | 2025-11-20 15:12:28.407Z | 333.017° NNW | 2025-11-20 15:16:28.407Z | 277.162° WNW | 26.345° | 2025-11-20 15:20:28.407Z | 228.195° WSW |
| 8 mins | 2025-11-21 01:18:28.407Z | 129.195° SE | 2025-11-21 01:22:28.407Z | 71.105° E | 26.574° | 2025-11-21 01:26:28.407Z | 21.65° NNE |
| 8 mins | 2025-11-21 03:03:28.407Z | 219.612° SW | 2025-11-21 03:07:28.407Z | 278.057° WNW | 28.195° | 2025-11-21 03:11:28.407Z | 332.619° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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