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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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: 21 hours ago
TLE from 21 hours ago
0 DELTA 1 DEB
1 2118U 66008D 26119.89965569 .00000445 00000-0 12272-3 0 9998
2 2118 98.0520 254.3377 0126026 11.6305 348.7752 14.46864479128844Epoch: 2026-04-29T21:35Z
TLE epoch observation values (Epoch: 2026-04-29T21:35:30.251Z)
Latitude
-0.00007°
Longitude
72.60767°
Altitude
650.965 km
Speed
7.579 km/s
True Right ascension
16h 57m 21s
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
02:31:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
822.618 km
Perigee altitude
643.381 km
Semi-major axis
7,111.136 km
Eccentricity
0.0126
Inclination
98.052°
RAAN
254.3377°
Arg. of periapsis
11.6305°
True anomaly
348.48968°
Mean anomaly
348.7752°
Eccentric anomaly
348.63288°
Mean motion
3.61938 °/min
Orbital period
99.46 mins
BSTAR
0.00012272
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-04-30 21:23:57.891Z | 26.075° NE | 2026-04-30 21:27:57.891Z | 91.295° ESE | 38.166° | 2026-04-30 21:32:57.891Z | 175.118° S |
| 5 mins | 2026-04-30 23:03:57.891Z | 326.489° NNW | 2026-04-30 23:05:57.891Z | 298.613° NW | 18.62° | 2026-04-30 23:08:57.891Z | 258.174° W |
| 7 mins | 2026-05-01 08:34:57.891Z | 143.146° SSE | 2026-05-01 08:37:57.891Z | 69.824° E | 38.565° | 2026-05-01 08:41:57.891Z | 358.255° N |
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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