ISS DEB, 69324 (Decayed)
Orbit data source: Space-Track
ISS DEB, 69324 was space debris in LEO that was on an ISS related-mission or a former payload that was launched from the ISS. 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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69324 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
RKKE
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
IRR, 0.1 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 ISS DEB
1 69324U 98067YG 26226.64297546 .05791217 11873-4 31596-2 0 9997
2 69324 51.6052 0.3255 0018780 316.0977 43.8547 16.18437754580951Epoch: 2026-08-14T15:25Z
TLE epoch observation values (Epoch: 2026-08-14T15:25:53.079Z)
Latitude
-0.00005°
Longitude
165.78903°
Altitude
215.627 km
Speed
7.784 km/s
True Right ascension
00h 01m 18s
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
01:48:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
236.725 km
Perigee altitude
211.926 km
Semi-major axis
6,602.462 km
Eccentricity
0.00188
Inclination
51.6052°
RAAN
0.3255°
Arg. of periapsis
316.0977°
True anomaly
44.00405°
Mean anomaly
43.8547°
Eccentric anomaly
43.92935°
Mean motion
4.04561 °/min
Orbital period
88.99 mins
BSTAR
0.0031596
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Other satellites on launch #67 in the year 1998 (1998-11-20 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.ISS 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
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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