SCOUT A DEB, 2386
Orbit data source: Space-Track
SCOUT A DEB, 2386 is space debris in LEO originally from a launch on Sat, 26 Mar 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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2386 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SCOUT A DEB
1 02386U 66024D 26154.25596513 .00000258 00000-0 21837-3 0 9990
2 02386 90.0365 331.2414 0128799 20.3863 340.2380 13.81613072320029Epoch: 2026-06-03T06:08Z
TLE epoch observation values (Epoch: 2026-06-03T06:08:35.387Z)
Latitude
-0°
Longitude
-12.62324°
Altitude
872.368 km
Speed
7.461 km/s
True Right ascension
22h 04m 57s
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
06:19:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,049.626 km
Perigee altitude
860.722 km
Semi-major axis
7,333.311 km
Eccentricity
0.01288
Inclination
90.0365°
RAAN
331.2414°
Arg. of periapsis
20.3863°
True anomaly
339.7313°
Mean anomaly
340.238°
Eccentric anomaly
339.98543°
Mean motion
3.45615 °/min
Orbital period
104.16 mins
BSTAR
0.00021837
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Other satellites on launch #24 in the year 1966 (1966-03-26 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 DEB 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-04 22:42:50.372Z | 36.772° NE | 2026-06-04 22:46:50.372Z | 77.454° E | 18.204° | 2026-06-04 22:50:50.372Z | 119.411° SE |
| 11 mins | 2026-06-05 00:26:50.372Z | 352.61° N | 2026-06-05 00:31:50.372Z | 259.584° W | 41.664° | 2026-06-05 00:37:50.372Z | 196.813° SSW |
| 9 mins | 2026-06-05 12:08:50.372Z | 179.232° S | 2026-06-05 12:12:50.372Z | 291.136° WNW | 44.868° | 2026-06-05 12:17:50.372Z | 356.375° N |
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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