ARIANE 5 R/B, 40148
Orbit data source: Space-Track
ARIANE 5 R/B, 40148 is space debris in HEO originally from a launch on Thu, 11 Sep 2014 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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
40148 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Create New Watchlist
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ARIANE 5 R/B
1 40148U 14054C 26061.73149079 .00009142 00000-0 20400-2 0 9990
2 40148 5.7498 83.8145 7040234 268.0419 17.3294 2.59286206101065Epoch: 2026-03-02T17:33Z
TLE epoch observation values (Epoch: 2026-03-02T17:33:20.804Z)
Latitude
-0.00001°
Longitude
20.38596°
Altitude
5,226.192 km
Speed
7.133 km/s
True Right ascension
05h 36m 58s
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
12:39:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
31,769.098 km
Perigee altitude
247.763 km
Semi-major axis
22,386.567 km
Eccentricity
0.70402
Inclination
5.7498°
RAAN
83.8145°
Arg. of periapsis
268.0419°
True anomaly
91.98008°
Mean anomaly
17.3294°
Eccentric anomaly
46.67289°
Mean motion
0.64798 °/min
Orbital period
555.57 mins
BSTAR
0.00204
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #54 in the year 2014 (2014-09-11 UTC)
Did you know?
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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 132 mins | 2026-03-03 08:55:32.484Z | 175.827° S | 2026-03-03 08:55:32.484Z | 175.827° S | 36.687° | 2026-03-03 11:07:32.484Z | 134.791° SE |
| 116 mins | 2026-03-04 06:59:32.484Z | 243.186° WSW | 2026-03-04 08:54:32.484Z | 234.051° WSW | 28.476° | 2026-03-04 08:55:32.484Z | 234.107° 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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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 |
|---|