MSG 4 DEB (BAFFLE COVER), 40990
Orbit data source: Space-Track
MSG 4 DEB (BAFFLE COVER), 40990 is space debris in GEO originally from a launch on Wed, 15 Jul 2015 UTC launched from the French Guiana (FRGUI). 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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40990 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 MSG 4 DEB (BAFFLE COVER)
1 40990U 15034F 26057.62012871 -.00000188 00000-0 00000+0 0 9999
2 40990 6.7437 80.4620 0098763 192.6237 167.2594 1.02662052 39767Epoch: 2026-02-26T14:52Z
TLE epoch observation values (Epoch: 2026-02-26T14:52:59.120Z)
Latitude
0.00001°
Longitude
60.90073°
Altitude
35,527.959 km
Speed
3.069 km/s
True Right ascension
05h 22m 27s
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
04:45:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,540.569 km
Perigee altitude
34,720.663 km
Semi-major axis
41,508.753 km
Eccentricity
0.00988
Inclination
6.7437°
RAAN
80.462°
Arg. of periapsis
192.6237°
True anomaly
167.50602°
Mean anomaly
167.2594°
Eccentric anomaly
167.383°
Mean motion
0.25665 °/min
Orbital period
1,402.71 mins
BSTAR
0
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Other satellites on launch #34 in the year 2015 (2015-07-15 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.MSG 4 DEB (BAFFLE COVER) 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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| MSG 4 DEB (BAFFLE COVER) is likely not visible in the next few days. |
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40990 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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