DELTA 1 DEB, 3126
Orbit data source: Space-Track
DELTA 1 DEB, 3126 is space debris in LEO originally from a launch on Thu, 11 Jan 1968 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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3126 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 DELTA 1 DEB
1 03126U 68002C 25284.35749517 -.00000070 00000-0 25350-4 0 9997
2 03126 106.0742 124.0918 0321936 196.0470 344.7092 12.82452231702389Epoch: 2025-10-11T08:34Z
TLE epoch observation values (Epoch: 2025-10-11T08:34:47.582Z)
Latitude
0.14171°
Longitude
155.24403°
Altitude
1,095.158 km
Speed
7.417 km/s
True Right ascension
20h 16m 31s
True Declination
0° 08' 27"
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
09:36:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,577.563 km
Perigee altitude
1,081.294 km
Semi-major axis
7,707.566 km
Eccentricity
0.03219
Inclination
106.0742°
RAAN
124.0918°
Arg. of periapsis
196.047°
True anomaly
343.69714°
Mean anomaly
344.7092°
Eccentric anomaly
344.20719°
Mean motion
3.2075 °/min
Orbital period
112.24 mins
BSTAR
0.00002535
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Other satellites on launch #2 in the year 1968 (1968-01-11 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 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-16 15:02:28.954Z | 223.491° SW | 2025-10-16 15:07:28.954Z | 258.439° W | 16.97° | 2025-10-16 15:12:28.954Z | 296.422° NW |
| 12 mins | 2025-10-17 02:48:28.954Z | 25.545° NE | 2025-10-17 02:54:28.954Z | 118.279° SE | 44.678° | 2025-10-17 03:00:28.954Z | 200.312° SSW |
| 8 mins | 2025-10-17 04:39:28.954Z | 350.562° N | 2025-10-17 04:43:28.954Z | 311.08° NW | 20.295° | 2025-10-17 04:47:28.954Z | 271.609° WNW |
| 12 mins | 2025-10-17 11:42:28.954Z | 105.149° ESE | 2025-10-17 11:48:28.954Z | 50.612° ENE | 29.062° | 2025-10-17 11:54:28.954Z | 357.202° N |
| 15 mins | 2025-10-17 13:30:28.954Z | 170.604° S | 2025-10-17 13:37:28.954Z | 252.782° W | 42.52° | 2025-10-17 13:45:28.954Z | 331.14° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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