INTELSAT 29E DEB, 62723
Orbit data source: Space-Track
INTELSAT 29E DEB, 62723 is space debris in GEO originally from a launch on Wed, 27 Jan 2016 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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62723 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ITSORelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 INTELSAT 29E DEB
1 62723U 16004E 25086.52352323 .00000010 00000-0 00000-0 0 9998
2 62723 5.4043 75.8258 0623060 307.4539 47.2101 1.00540659 8060Epoch: 2025-03-27T12:33Z
TLE epoch observation values (Epoch: 2025-03-27T12:33:52.407Z)
Latitude
-0.00089°
Longitude
62.38968°
Altitude
34,024.021 km
Speed
3.203 km/s
True Right ascension
05h 04m 12s
True Declination
0° 00' 03"
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
23:32:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,334.948 km
Perigee altitude
33,089.956 km
Semi-major axis
42,090.589 km
Eccentricity
0.06231
Inclination
5.4043°
RAAN
75.8258°
Arg. of periapsis
307.4539°
True anomaly
52.73297°
Mean anomaly
47.2101°
Eccentric anomaly
49.94247°
Mean motion
0.25134 °/min
Orbital period
1,432.31 mins
BSTAR
0
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Other satellites on launch #4 in the year 2016 (2016-01-27 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.INTELSAT 29E DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-09-16 06:51:29.757Z | 235.694° WSW | 2025-09-16 19:18:29.757Z | 229.769° WSW | 31.578° | 2025-09-17 06:51:29.757Z | 234.733° WSW |
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62723 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 ascending 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 ascending order |
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