DELTA 1 DEB, 12226 (Decayed)
Orbit data source: Space-Track
DELTA 1 DEB, 12226 was space debris in SSO originally from a launch on Sun, 05 Mar 1978 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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12226 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 DELTA 1 DEB
1 12226U 78026BT 25094.24765499 .04431788 00000-0 47549-1 0 9997
2 12226 98.8541 191.7305 0030073 304.6766 55.1652 15.58871406227898Epoch: 2025-04-04T05:56Z
TLE epoch observation values (Epoch: 2025-04-04T05:56:37.391Z)
Latitude
-0.00002°
Longitude
-90.23417°
Altitude
382.43 km
Speed
7.687 km/s
True Right ascension
12h 46m 55s
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
09:52:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
408.253 km
Perigee altitude
367.558 km
Semi-major axis
6,766.042 km
Eccentricity
0.00301
Inclination
98.8541°
RAAN
191.7305°
Arg. of periapsis
304.6766°
True anomaly
55.44867°
Mean anomaly
55.1652°
Eccentric anomaly
55.30687°
Mean motion
3.89979 °/min
Orbital period
92.31 mins
BSTAR
0.047549
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Other satellites on launch #26 in the year 1978 (1978-03-05 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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