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
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 25312.36733492 .00000158 00000-0 15068-3 0 9992
2 1953 90.1482 349.2741 0229184 119.3068 243.1205 13.65021215972751Epoch: 2025-11-08T08:48Z
TLE epoch observation values (Epoch: 2025-11-08T08:48:57.737Z)
Latitude
-0°
Longitude
169.23557°
Altitude
1,100.17 km
Speed
7.263 km/s
True Right ascension
23h 17m 05s
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
17:41:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,183.953 km
Perigee altitude
845.097 km
Semi-major axis
7,392.662 km
Eccentricity
0.02292
Inclination
90.1482°
RAAN
349.2741°
Arg. of periapsis
119.3068°
True anomaly
240.80858°
Mean anomaly
243.1205°
Eccentric anomaly
241.96149°
Mean motion
3.41462 °/min
Orbital period
105.43 mins
BSTAR
0.00015068
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-09 02:30:39.933Z | 157.633° S | 2025-11-09 02:36:39.933Z | 72.567° E | 39.281° | 2025-11-09 02:41:39.933Z | 8.333° NNE |
| 7 mins | 2025-11-09 04:18:39.933Z | 240.905° WSW | 2025-11-09 04:21:39.933Z | 274.277° WNW | 19.331° | 2025-11-09 04:25:39.933Z | 320.202° NNW |
| 5 mins | 2025-11-09 13:35:39.933Z | 55.514° ENE | 2025-11-09 13:37:39.933Z | 79.949° E | 15.478° | 2025-11-09 13:40:39.933Z | 114.159° SE |
| 9 mins | 2025-11-09 15:19:39.933Z | 349.144° N | 2025-11-09 15:23:39.933Z | 262.424° W | 40.168° | 2025-11-09 15:28:39.933Z | 199.345° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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