DELTA 1 DEB, 10177
Orbit data source: Space-Track
DELTA 1 DEB, 10177 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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10177 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 DELTA 1 DEB
1 10177U 77065F 25300.51788369 .00005022 00000-0 75463-3 0 9995
2 10177 28.2295 20.1456 0480404 110.6370 254.6370 14.16542962263987Epoch: 2025-10-27T12:25Z
TLE epoch observation values (Epoch: 2025-10-27T12:25:45.150Z)
Latitude
-0.00005°
Longitude
157.5888°
Altitude
942.358 km
Speed
7.328 km/s
True Right ascension
01h 20m 34s
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
12:43:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,187.961 km
Perigee altitude
494.327 km
Semi-major axis
7,219.281 km
Eccentricity
0.04804
Inclination
28.2295°
RAAN
20.1456°
Arg. of periapsis
110.637°
True anomaly
249.41908°
Mean anomaly
254.637°
Eccentric anomaly
252.01892°
Mean motion
3.53836 °/min
Orbital period
101.74 mins
BSTAR
0.00075463
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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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