SCOUT A R/B, 1865
Orbit data source: Space-Track
SCOUT A R/B, 1865 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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1865 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 SCOUT A R/B
1 1865U 65109B 25332.07441863 .00000148 00000-0 13292-3 0 9992
2 1865 89.0650 268.8737 0109680 232.5891 126.5253 13.76782203 5968Epoch: 2025-11-28T01:47Z
TLE epoch observation values (Epoch: 2025-11-28T01:47:09.769Z)
Latitude
-0.00009°
Longitude
174.8608°
Altitude
1,026.891 km
Speed
7.314 km/s
True Right ascension
17h 55m 29s
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
15:12:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,052.955 km
Perigee altitude
891.715 km
Semi-major axis
7,350.472 km
Eccentricity
0.01097
Inclination
89.065°
RAAN
268.8737°
Arg. of periapsis
232.5891°
True anomaly
127.52706°
Mean anomaly
126.5253°
Eccentric anomaly
127.027°
Mean motion
3.44406 °/min
Orbital period
104.53 mins
BSTAR
0.00013292
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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 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 | 2025-11-28 19:20:35.066Z | 135.632° SSE | 2025-11-28 19:25:35.066Z | 83.913° E | 27.058° | 2025-11-28 19:30:35.066Z | 24.485° NE |
| 10 mins | 2025-11-28 21:05:35.066Z | 211.732° SW | 2025-11-28 21:10:35.066Z | 283.03° WNW | 33.742° | 2025-11-28 21:15:35.066Z | 341.749° N |
| 11 mins | 2025-11-29 08:02:35.066Z | 5.938° NNE | 2025-11-29 08:07:35.066Z | 82.865° E | 43.941° | 2025-11-29 08:13:35.066Z | 175.509° S |
| 5 mins | 2025-11-29 09:49:35.066Z | 307.404° NW | 2025-11-29 09:51:35.066Z | 285.675° WNW | 15.053° | 2025-11-29 09:54:35.066Z | 255.322° W |
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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