DELTA 1 DEB, 10234
Orbit data source: Space-Track
DELTA 1 DEB, 10234 is space debris in LEO originally from a launch on Thu, 14 Jul 1977 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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10234 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 DELTA 1 DEB
1 10234U 77065BM 25297.96470009 .00026545 00000-0 19844-2 0 9995
2 10234 28.9446 198.4306 0296932 49.9901 312.6360 14.72612729446151Epoch: 2025-10-24T23:09Z
TLE epoch observation values (Epoch: 2025-10-24T23:09:10.087Z)
Latitude
-0.00004°
Longitude
177.53645°
Altitude
513.166 km
Speed
7.684 km/s
True Right ascension
13h 13m 43s
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
02:04:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
865.705 km
Perigee altitude
447.924 km
Semi-major axis
7,034.951 km
Eccentricity
0.02969
Inclination
28.9446°
RAAN
198.4306°
Arg. of periapsis
49.9901°
True anomaly
310.06919°
Mean anomaly
312.636°
Eccentric anomaly
311.35904°
Mean motion
3.67834 °/min
Orbital period
97.87 mins
BSTAR
0.0019844
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Other satellites on launch #65 in the year 1977 (1977-07-14 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.DELTA 1 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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| DELTA 1 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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