DELTA 1 DEB, 10227
Orbit data source: Space-Track
DELTA 1 DEB, 10227 is space debris in LEO originally from a launch on Thu, 14 Jul 1977 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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10227 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.6 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 DELTA 1 DEB
1 10227U 77065BE 25351.90719473 .00002486 00000-0 80379-3 0 9993
2 10227 28.9485 175.2919 0675226 176.9226 183.5774 13.52549849350110Epoch: 2025-12-17T21:46Z
TLE epoch observation values (Epoch: 2025-12-17T21:46:21.624Z)
Latitude
-0.00003°
Longitude
121.93142°
Altitude
1,562.762 km
Speed
6.846 km/s
True Right ascension
11h 41m 10s
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
10:01:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,569.462 km
Perigee altitude
564.064 km
Semi-major axis
7,444.9 km
Eccentricity
0.06752
Inclination
28.9485°
RAAN
175.2919°
Arg. of periapsis
176.9226°
True anomaly
183.13222°
Mean anomaly
183.5774°
Eccentric anomaly
183.35124°
Mean motion
3.37874 °/min
Orbital period
106.55 mins
BSTAR
0.00080379
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Other satellites on launch #65 in the year 1977 (1977-07-14 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 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-18 15:41:56.874Z | 206.832° SW | 2025-12-18 15:47:56.874Z | 160.449° S | 22.685° | 2025-12-18 15:52:56.874Z | 116.967° SE |
| 11 mins | 2025-12-18 17:34:56.874Z | 231.849° WSW | 2025-12-18 17:40:56.874Z | 175.689° S | 29.066° | 2025-12-18 17:45:56.874Z | 119.716° SE |
| 9 mins | 2025-12-18 19:28:56.874Z | 242.302° WSW | 2025-12-18 19:33:56.874Z | 188.239° SSW | 25.575° | 2025-12-18 19:37:56.874Z | 139.11° SSE |
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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