ARIANE 5 R/B, 41030
Orbit data source: Space-Track
ARIANE 5 R/B, 41030 is space debris in HEO originally from a launch on Tue, 10 Nov 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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41030 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
Airbus Safran
Mission
Spacecraft
Bus & Motor
ESC-A, Unknown motor
Mass
~5,000 kg wet, ~5,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 3.5 m
Radar Cross Section
41.627 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ARIANE 5 R/B
1 41030U 15065C 26251.08914820 .00005603 00000-0 10008-2 0 9998
2 41030 4.0865 239.8158 7029941 63.6742 350.5322 2.61171246 94899Epoch: 2026-09-08T02:08Z
TLE epoch observation values (Epoch: 2026-09-08T02:08:22.404Z)
Latitude
-0.00003°
Longitude
-139.9593°
Altitude
2,242.53 km
Speed
8.635 km/s
True Right ascension
15h 57m 10s
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
09:25:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
31,562.508 km
Perigee altitude
238.795 km
Semi-major axis
22,278.788 km
Eccentricity
0.70299
Inclination
4.0865°
RAAN
239.8158°
Arg. of periapsis
63.6742°
True anomaly
296.48515°
Mean anomaly
350.5322°
Eccentric anomaly
331.01233°
Mean motion
0.65269 °/min
Orbital period
551.56 mins
BSTAR
0.0010008
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Other satellites on launch #65 in the year 2015 (2015-11-10 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.ARIANE 5 R/B 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. |
|---|---|---|---|---|---|---|---|
| 184 mins | 2026-09-08 17:14:46.821Z | 189.886° SSW | 2026-09-08 17:14:46.821Z | 189.886° SSW | 37.771° | 2026-09-08 20:18:46.821Z | 146.475° SSE |
| 54 mins | 2026-09-09 16:20:46.821Z | 242.139° WSW | 2026-09-09 17:14:46.821Z | 236.547° WSW | 18.404° | 2026-09-09 17:14:46.821Z | 236.547° WSW |
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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