DELTA 1 DEB (YO), 312
Orbit data source: Space-Track
DELTA 1 DEB (YO), 312 is space debris in LEO originally from a launch on Tue, 19 Jun 1962 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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312 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 DELTA 1 DEB (YO)
1 312U 62025C 26036.69061185 .00003304 00000-0 53632-3 0 9996
2 312 58.2457 146.8867 0195539 128.7342 233.1351 14.61564774339691Epoch: 2026-02-05T16:34Z
TLE epoch observation values (Epoch: 2026-02-05T16:34:28.863Z)
Latitude
-0.00001°
Longitude
122.42721°
Altitude
774.112 km
Speed
7.423 km/s
True Right ascension
09h 47m 32s
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
14:20:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.766 km
Perigee altitude
549.44 km
Semi-major axis
7,065.74 km
Eccentricity
0.01955
Inclination
58.2457°
RAAN
146.8867°
Arg. of periapsis
128.7342°
True anomaly
231.36861°
Mean anomaly
233.1351°
Eccentric anomaly
232.24926°
Mean motion
3.65432 °/min
Orbital period
98.51 mins
BSTAR
0.00053632
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Other satellites on launch #25 in the year 1962 (1962-06-19 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 (YO) 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-06 16:02:44.256Z | 343.06° N | 2026-02-06 16:05:44.256Z | 30.611° NE | 20.472° | 2026-02-06 16:08:44.256Z | 83.376° E |
| 6 mins | 2026-02-06 17:45:44.256Z | 299.292° NW | 2026-02-06 17:47:44.256Z | 255.421° W | 35.58° | 2026-02-06 17:51:44.256Z | 160.431° S |
| 5 mins | 2026-02-07 08:07:44.256Z | 156.415° SSE | 2026-02-07 08:09:44.256Z | 122.819° SE | 22.261° | 2026-02-07 08:12:44.256Z | 75.563° E |
| 7 mins | 2026-02-07 09:48:44.256Z | 249.936° W | 2026-02-07 09:51:44.256Z | 318.464° NNW | 36.709° | 2026-02-07 09:55:44.256Z | 30.32° NE |
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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