THORAD DELTA 1 DEB, 8561
Orbit data source: Space-Track
THORAD DELTA 1 DEB, 8561 is space debris in SSO originally from a launch on Fri, 15 Nov 1974 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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8561 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 THORAD DELTA 1 DEB
1 08561U 74089CY 25300.03368894 .00000565 00000-0 31541-2 0 9991
2 08561 101.5228 338.8765 0067770 272.8784 117.7415 12.67481955345776Epoch: 2025-10-27T00:48Z
TLE epoch observation values (Epoch: 2025-10-27T00:48:30.724Z)
Latitude
30.65646°
Longitude
-75.79891°
Altitude
1,420.616 km
Speed
7.142 km/s
True Right ascension
22h 07m 52s
True Declination
30° 31' 07"
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
19:04:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,442.368 km
Perigee altitude
1,337.082 km
Semi-major axis
7,767.862 km
Eccentricity
0.00678
Inclination
101.5228°
RAAN
338.8765°
Arg. of periapsis
272.8784°
True anomaly
118.42611°
Mean anomaly
117.7415°
Eccentric anomaly
118.08407°
Mean motion
3.17023 °/min
Orbital period
113.56 mins
BSTAR
0.0031541
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Other satellites on launch #89 in the year 1974 (1974-11-15 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.THORAD 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2025-10-28 01:24:02.909Z | 123.442° SE | 2025-10-28 01:31:02.909Z | 55.792° ENE | 32.381° | 2025-10-28 01:38:02.909Z | 356.942° N |
| 13 mins | 2025-10-28 03:16:02.909Z | 192.381° SSW | 2025-10-28 03:22:02.909Z | 258.397° W | 36.364° | 2025-10-28 03:29:02.909Z | 329.096° NNW |
| 14 mins | 2025-10-28 15:10:02.909Z | 28.442° NE | 2025-10-28 15:17:02.909Z | 110.76° ESE | 39.653° | 2025-10-28 15:24:02.909Z | 178.508° S |
| 12 mins | 2025-10-28 17:02:02.909Z | 355.669° N | 2025-10-28 17:08:02.909Z | 299.006° NW | 29.113° | 2025-10-28 17:14:02.909Z | 244.651° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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