OPS 5960 DEB, 43000
Orbit data source: Space-Track
OPS 5960 DEB, 43000 is space debris originally from a launch on Fri, 06 Nov 1970 UTC launched from the Air Force Eastern Test Range (AFETR). 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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43000 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OPS 5960 DEB
1 43000U 70093D 26170.61450784 -.00000155 00000-0 00000-0 0 9999
2 43000 15.2208 35.7965 1167554 276.0860 70.7360 1.20560077 45651Epoch: 2026-06-19T14:44Z
TLE epoch observation values (Epoch: 2026-06-19T14:44:53.477Z)
Latitude
0.00001°
Longitude
-93.26084°
Altitude
29,970.133 km
Speed
3.353 km/s
True Right ascension
02h 23m 12s
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
21:31:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,267.587 km
Perigee altitude
26,559.569 km
Semi-major axis
37,291.715 km
Eccentricity
0.11676
Inclination
15.2208°
RAAN
35.7965°
Arg. of periapsis
276.086°
True anomaly
83.88652°
Mean anomaly
70.736°
Eccentric anomaly
77.26092°
Mean motion
0.30139 °/min
Orbital period
1,194.48 mins
BSTAR
0
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Other satellites on launch #93 in the year 1970 (1970-11-06 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 5960 DEB Visibility
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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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| OPS 5960 DEB is likely not visible in the next few days. |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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