W-SERIES 4 DEB, 69094 (Decayed)
Orbit data source: Space-Track
W-SERIES 4 DEB, 69094 was space debris in LEO originally from a launch on Mon, 23 Jun 2025 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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69094 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Varda Space
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 W-SERIES 4 DEB
1 69094U 25135BX 26138.34724196 .22786312 10859-5 67873-3 0 9993
2 69094 97.4279 249.6800 0098028 195.7097 164.1151 16.28547179 2115Epoch: 2026-05-18T08:20Z
TLE epoch observation values (Epoch: 2026-05-18T08:20:01.705Z)
Latitude
0.00002°
Longitude
-111.36391°
Altitude
261.732 km
Speed
7.713 km/s
True Right ascension
16h 38m 43s
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
06:55:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
257.688 km
Perigee altitude
128.852 km
Semi-major axis
6,571.407 km
Eccentricity
0.0098
Inclination
97.4279°
RAAN
249.68°
Arg. of periapsis
195.7097°
True anomaly
164.41897°
Mean anomaly
164.1151°
Eccentric anomaly
164.26739°
Mean motion
4.07432 °/min
Orbital period
88.36 mins
BSTAR
0.00067873
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Other satellites on launch #135 in the year 2025 (2025-06-23 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.W-SERIES 4 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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