COSMOS 1700 DEB, 40924
Orbit data source: Space-Track
COSMOS 1700 DEB, 40924 is space debris in GEO originally from a launch on Fri, 25 Oct 1985 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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40924 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 COSMOS 1700 DEB
1 40924U 85102G 26069.24142075 .00000015 00000-0 00000-0 0 9999
2 40924 9.8565 319.3979 0021758 119.3165 240.7135 1.00216937 66434Epoch: 2026-03-10T05:47Z
TLE epoch observation values (Epoch: 2026-03-10T05:47:38.752Z)
Latitude
-0.02757°
Longitude
64.41093°
Altitude
35,846.313 km
Speed
3.071 km/s
True Right ascension
21h 16m 58s
True Declination
0° 01' 39"
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
20:12:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,894.78 km
Perigee altitude
35,711.224 km
Semi-major axis
42,181.139 km
Eccentricity
0.00218
Inclination
9.8565°
RAAN
319.3979°
Arg. of periapsis
119.3165°
True anomaly
240.49633°
Mean anomaly
240.7135°
Eccentric anomaly
240.60489°
Mean motion
0.25053 °/min
Orbital period
1,436.93 mins
BSTAR
0
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Other satellites on launch #102 in the year 1985 (1985-10-25 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.COSMOS 1700 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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| COSMOS 1700 DEB is likely not visible in the next few days. |
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40924 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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