WORLDVIEW 2 DEB, 41736 (Decayed)
Orbit data source: Space-Track
WORLDVIEW 2 DEB, 41736 was space debris in SSO originally from a launch on Thu, 08 Oct 2009 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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41736 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Ball
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 WORLDVIEW 2 DEB
1 41736U 09055D 24280.31310700 .09685552 21750+0 43330-1 0 9999
2 41736 98.4323 40.2021 0028343 312.9526 46.9367 15.91500427433648Epoch: 2024-10-06T07:30Z
TLE epoch observation values (Epoch: 2024-10-06T07:30:52.444Z)
Latitude
-0.00007°
Longitude
-87.97327°
Altitude
288.343 km
Speed
7.742 km/s
True Right ascension
02h 40m 48s
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
02:12:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
313.917 km
Perigee altitude
276.089 km
Semi-major axis
6,673.14 km
Eccentricity
0.00283
Inclination
98.4323°
RAAN
40.2021°
Arg. of periapsis
312.9526°
True anomaly
47.17456°
Mean anomaly
46.9367°
Eccentric anomaly
47.05557°
Mean motion
3.98151 °/min
Orbital period
90.42 mins
BSTAR
0.04333
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Other satellites on launch #55 in the year 2009 (2009-10-08 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.WORLDVIEW 2 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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