OPS 4682 DEB, 38386
Orbit data source: Space-Track
OPS 4682 DEB, 38386 is space debris in LEO originally from a launch on Sat, 03 Apr 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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38386 intel report (Beta)
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Edit Public Description
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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OPS 4682 DEB
1 38386U 65027CP 25300.53906787 .00001280 00000-0 41496-2 0 9990
2 38386 90.2798 27.9144 0034347 112.1797 248.2976 13.01150003627413Epoch: 2025-10-27T12:56Z
TLE epoch observation values (Epoch: 2025-10-27T12:56:15.463Z)
Latitude
-0.00006°
Longitude
157.71051°
Altitude
1,270.247 km
Speed
7.216 km/s
True Right ascension
01h 51m 39s
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
10:37:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,280.926 km
Perigee altitude
1,228.493 km
Semi-major axis
7,632.846 km
Eccentricity
0.00343
Inclination
90.2798°
RAAN
27.9144°
Arg. of periapsis
112.1797°
True anomaly
247.93249°
Mean anomaly
248.2976°
Eccentric anomaly
248.11499°
Mean motion
3.25472 °/min
Orbital period
110.61 mins
BSTAR
0.0041496
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Other satellites on launch #27 in the year 1965 (1965-04-03 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.OPS 4682 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-29 17:13:46.188Z | 23.22° NE | 2025-10-29 17:19:46.188Z | 86.628° E | 29.995° | 2025-10-29 17:25:46.188Z | 145.987° SSE |
| 12 mins | 2025-10-29 19:04:46.188Z | 342.762° N | 2025-10-29 19:09:46.188Z | 286.614° WNW | 33.541° | 2025-10-29 19:16:46.188Z | 214.939° SW |
| 12 mins | 2025-10-30 05:38:46.188Z | 152.606° SSE | 2025-10-30 05:44:46.188Z | 69.514° E | 39.452° | 2025-10-30 05:50:46.188Z | 7.844° NNE |
| 10 mins | 2025-10-30 07:30:46.188Z | 234.541° WSW | 2025-10-30 07:34:46.188Z | 274.575° WNW | 23.875° | 2025-10-30 07:40:46.188Z | 331.775° 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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