OPS 4682 DEB, 18964
Orbit data source: Space-Track
OPS 4682 DEB, 18964 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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18964 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OPS 4682 DEB
1 18964U 65027AM 26036.34810726 .00000515 00000-0 17402-2 0 9993
2 18964 90.2449 356.9365 0033608 88.7001 66.0883 12.97663860838366Epoch: 2026-02-05T08:21Z
TLE epoch observation values (Epoch: 2026-02-05T08:21:16.467Z)
Latitude
24.88333°
Longitude
-83.77072°
Altitude
1,263.91 km
Speed
7.23 km/s
True Right ascension
11h 48m 11s
True Declination
24° 45' 40"
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
20:02:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,294.082 km
Perigee altitude
1,242.685 km
Semi-major axis
7,646.521 km
Eccentricity
0.00336
Inclination
90.2449°
RAAN
356.9365°
Arg. of periapsis
88.7001°
True anomaly
66.44096°
Mean anomaly
66.0883°
Eccentric anomaly
66.26457°
Mean motion
3.24599 °/min
Orbital period
110.91 mins
BSTAR
0.0017402
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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 | 2026-02-05 20:37:54.859Z | 135.816° SSE | 2026-02-05 20:43:54.859Z | 72.65° E | 30.478° | 2026-02-05 20:49:54.859Z | 15.554° NNE |
| 12 mins | 2026-02-05 22:28:54.859Z | 212.627° SW | 2026-02-05 22:33:54.859Z | 268.956° W | 33.396° | 2026-02-05 22:40:54.859Z | 342.665° N |
| 10 mins | 2026-02-06 08:14:54.859Z | 33.527° NE | 2026-02-06 08:19:54.859Z | 81.688° E | 22.741° | 2026-02-06 08:24:54.859Z | 128.181° SE |
| 13 mins | 2026-02-06 10:04:54.859Z | 352.395° N | 2026-02-06 10:10:54.859Z | 278.003° WNW | 40.8° | 2026-02-06 10:17:54.859Z | 201.648° SSW |
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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