SCOUT A R/B, 2180
Orbit data source: Space-Track
SCOUT A R/B, 2180 is space debris in LEO originally from a launch on Thu, 19 May 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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2180 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 02180U 66041B 25256.74824265 .00000025 00000-0 90820-5 0 9997
2 02180 90.2182 75.7611 0080034 112.6742 248.2925 14.00981297 24560
Epoch: 2025-09-13T17:57Z
TLE epoch observation values (Epoch: 2025-09-13T17:57:28.164Z)
Latitude
-0.00005°
Longitude
173.4166°
Altitude
915.348 km
Speed
7.383 km/s
True Right ascension
05h 03m 02s
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
00:44:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
945.524 km
Perigee altitude
829.226 km
Semi-major axis
7,265.512 km
Eccentricity
0.008
Inclination
90.2182°
RAAN
75.7611°
Arg. of periapsis
112.6742°
True anomaly
247.44359°
Mean anomaly
248.2925°
Eccentric anomaly
247.86773°
Mean motion
3.50464 °/min
Orbital period
102.72 mins
BSTAR
0.000009082
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Other satellites on launch #41 in the year 1966 (1966-05-19 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. |
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8 mins | 2025-09-14 11:13:46.485Z | 123.345° SE | 2025-09-14 11:17:46.485Z | 77.71° E | 20.411° | 2025-09-14 11:21:46.485Z | 29.358° NE |
9 mins | 2025-09-14 12:55:46.485Z | 202.587° SW | 2025-09-14 12:59:46.485Z | 259.348° W | 35.695° | 2025-09-14 13:04:46.485Z | 342.217° N |
8 mins | 2025-09-14 23:41:46.485Z | 26.781° NE | 2025-09-14 23:45:46.485Z | 93.122° ESE | 31.09° | 2025-09-14 23:49:46.485Z | 149.695° SSE |
7 mins | 2025-09-15 01:24:46.485Z | 327.302° NNW | 2025-09-15 01:27:46.485Z | 285.333° WNW | 23.344° | 2025-09-15 01:31:46.485Z | 232.845° WSW |
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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