DELTA 1 DEB (YO), 228
Orbit data source: Space-Track
DELTA 1 DEB (YO), 228 is space debris in LEO originally from a launch on Thu, 08 Feb 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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228 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 DELTA 1 DEB (YO)
1 00228U 62002C 26035.09783861 .00030009 00000-0 66093-3 0 9999
2 00228 48.4319 300.5773 0007355 209.0937 150.9595 15.43569253422485Epoch: 2026-02-04T02:20Z
TLE epoch observation values (Epoch: 2026-02-04T02:20:53.255Z)
Latitude
-0.00003°
Longitude
131.08607°
Altitude
440.351 km
Speed
7.647 km/s
True Right ascension
20h 02m 18s
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
00:59:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.638 km
Perigee altitude
431.614 km
Semi-major axis
6,814.763 km
Eccentricity
0.00074
Inclination
48.4319°
RAAN
300.5773°
Arg. of periapsis
209.0937°
True anomaly
151.00038°
Mean anomaly
150.9595°
Eccentric anomaly
150.97994°
Mean motion
3.85804 °/min
Orbital period
93.31 mins
BSTAR
0.00066093
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Other satellites on launch #2 in the year 1962 (1962-02-08 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-05 00:29:04.192Z | 319.202° NNW | 2026-02-05 00:32:04.192Z | 22.683° NE | 19.905° | 2026-02-05 00:34:04.192Z | 59.878° ENE |
| 4 mins | 2026-02-05 02:08:04.192Z | 317.686° NNW | 2026-02-05 02:09:04.192Z | 348.802° N | 39.671° | 2026-02-05 02:12:04.192Z | 107.602° ESE |
| 5 mins | 2026-02-05 20:31:04.192Z | 237.927° WSW | 2026-02-05 20:33:04.192Z | 58.694° ENE | 43.537° | 2026-02-05 20:36:04.192Z | 58.874° ENE |
| 4 mins | 2026-02-05 22:09:04.192Z | 309.001° NW | 2026-02-05 22:10:04.192Z | 333.218° NNW | 22.189° | 2026-02-05 22:13:04.192Z | 40.14° 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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