DELTA 1 DEB, 2118
Orbit data source: Space-Track
DELTA 1 DEB, 2118 is space debris in SSO originally from a launch on Thu, 03 Feb 1966 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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2118 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~1 kg wet, ~1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 DELTA 1 DEB
1 02118U 66008D 25336.33950014 .00001073 00000-0 28004-3 0 9994
2 02118 98.0315 113.2413 0127596 106.4642 255.0617 14.46585608107368Epoch: 2025-12-02T08:08Z
TLE epoch observation values (Epoch: 2025-12-02T08:08:52.812Z)
Latitude
-0.00001°
Longitude
-80.40481°
Altitude
764.278 km
Speed
7.459 km/s
True Right ascension
07h 32m 57s
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
05:14:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
824.66 km
Perigee altitude
643.166 km
Semi-major axis
7,112.05 km
Eccentricity
0.01276
Inclination
98.0315°
RAAN
113.2413°
Arg. of periapsis
106.4642°
True anomaly
253.6549°
Mean anomaly
255.0617°
Eccentric anomaly
254.3577°
Mean motion
3.61869 °/min
Orbital period
99.48 mins
BSTAR
0.00028004
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Other satellites on launch #8 in the year 1966 (1966-02-03 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-03 09:10:05.015Z | 160.455° S | 2025-12-03 09:14:05.015Z | 82.362° E | 44.345° | 2025-12-03 09:18:05.015Z | 350.868° N |
| 5 mins | 2025-12-03 21:17:05.015Z | 66.941° ENE | 2025-12-03 21:19:05.015Z | 104.863° ESE | 20.758° | 2025-12-03 21:22:05.015Z | 146.332° SSE |
| 6 mins | 2025-12-03 22:55:05.015Z | 333.522° NNW | 2025-12-03 22:57:05.015Z | 289.978° WNW | 27.645° | 2025-12-03 23:01:05.015Z | 228.074° WSW |
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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