OPS 4682 DEB, 18270
Orbit data source: Space-Track
OPS 4682 DEB, 18270 is space debris in LEO originally from a launch on Sat, 03 Apr 1965 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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18270 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, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OPS 4682 DEB
1 18270U 65027Z 25295.16915023 .00000881 00000-0 30226-2 0 9990
2 18270 90.2362 354.5509 0028023 10.7566 45.5449 12.97066318885738Epoch: 2025-10-22T04:03Z
TLE epoch observation values (Epoch: 2025-10-22T04:03:34.579Z)
Latitude
56.62117°
Longitude
-97.5465°
Altitude
1,268.138 km
Speed
7.234 km/s
True Right ascension
23h 36m 46s
True Declination
56° 28' 25"
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
15:29:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,292.168 km
Perigee altitude
1,249.3 km
Semi-major axis
7,648.871 km
Eccentricity
0.0028
Inclination
90.2362°
RAAN
354.5509°
Arg. of periapsis
10.7566°
True anomaly
45.77468°
Mean anomaly
45.5449°
Eccentric anomaly
45.65973°
Mean motion
3.2445 °/min
Orbital period
110.96 mins
BSTAR
0.0030226
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Other satellites on launch #27 in the year 1965 (1965-04-03 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.OPS 4682 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 | 2025-10-23 03:55:34.188Z | 158.683° S | 2025-10-23 04:02:34.188Z | 86.684° E | 40.793° | 2025-10-23 04:09:34.188Z | 5.838° NNE |
| 10 mins | 2025-10-23 05:49:34.188Z | 237.143° WSW | 2025-10-23 05:53:34.188Z | 276.113° WNW | 22.643° | 2025-10-23 05:59:34.188Z | 331.25° NNW |
| 12 mins | 2025-10-23 15:34:34.188Z | 23.251° NE | 2025-10-23 15:39:34.188Z | 79.241° E | 33.946° | 2025-10-23 15:46:34.188Z | 153.356° SSE |
| 11 mins | 2025-10-23 17:25:34.188Z | 337.747° N | 2025-10-23 17:30:34.188Z | 281.819° WNW | 30.715° | 2025-10-23 17:36:34.188Z | 223.308° SW |
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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