DELTA 1 DEB *, 10395 (Decayed)
Orbit data source: Space-Track
DELTA 1 DEB *, 10395 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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10395 intel report (Beta)
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Edit Public Description
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: 9 months ago
TLE from 9 months ago
0 DELTA 1 DEB *
1 10395U 73086GK 25018.41752771 .36362174 00000-0 27371+0 0 9993
2 10395 102.6608 338.6439 0015716 153.1875 207.0179 15.64652320318281Epoch: 2025-01-18T10:01Z
TLE epoch observation values (Epoch: 2025-01-18T10:01:14.394Z)
Latitude
-0.00005°
Longitude
70.26683°
Altitude
386.643 km
Speed
7.673 km/s
True Right ascension
22h 34m 34s
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
16:42:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
382.06 km
Perigee altitude
360.845 km
Semi-major axis
6,749.59 km
Eccentricity
0.00157
Inclination
102.6608°
RAAN
338.6439°
Arg. of periapsis
153.1875°
True anomaly
206.93623°
Mean anomaly
207.0179°
Eccentric anomaly
206.97705°
Mean motion
3.91406 °/min
Orbital period
91.98 mins
BSTAR
0.27371
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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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