DELTA 1 DEB, 42580 (Decayed)
Orbit data source: Space-Track
DELTA 1 DEB, 42580 was space debris in SSO originally from a launch on Tue, 06 Nov 1973 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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42580 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Decayed 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: 2 months ago
TLE from 2 months ago
0 DELTA 1 DEB
1 42580U 73086HU 26144.66367812 .00335820 00000-0 21372-1 0 9996
2 42580 101.4397 223.3603 0009300 202.6298 157.4507 15.07013217632104Epoch: 2026-05-24T15:55Z
TLE epoch observation values (Epoch: 2026-05-24T15:55:41.789Z)
Latitude
-0.00002°
Longitude
102.1736°
Altitude
554.209 km
Speed
7.581 km/s
True Right ascension
14h 53m 26s
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
16:01:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
548.969 km
Perigee altitude
536.096 km
Semi-major axis
6,920.67 km
Eccentricity
0.00093
Inclination
101.4397°
RAAN
223.3603°
Arg. of periapsis
202.6298°
True anomaly
157.49152°
Mean anomaly
157.4507°
Eccentric anomaly
157.47112°
Mean motion
3.76982 °/min
Orbital period
95.5 mins
BSTAR
0.021372
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Other satellites on launch #86 in the year 1973 (1973-11-06 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
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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