STELLA, 22824
Orbit data source: Space-Track
STELLA, 22824 is a payload satellite owned by CNES (FR) in SSO that was launched on Sun, 26 Sep 1993 UTC via an ARIANE 40 launch vehicle from the French Guiana (FRGUI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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22824 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
CNES
Mission
Operational Civil Geodetic
Bus & Motor
STARLETTE, Unknown motor
Mass
48 kg wet, 48 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Sphere, 0.1 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STELLA
1 22824U 93061B 25258.28907788 -.00000046 00000-0 -15578-6 0 9992
2 22824 98.8150 315.9777 0005685 324.9927 124.0699 14.27459181665550Epoch: 2025-09-15T06:56Z
TLE epoch observation values (Epoch: 2025-09-15T06:56:16.328Z)
Latitude
81.18729°
Longitude
133.16727°
Altitude
815.943 km
Speed
7.451 km/s
True Right ascension
15h 26m 55s
True Declination
81° 08' 08"
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
11:43:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
801.469 km
Perigee altitude
793.311 km
Semi-major axis
7,175.527 km
Eccentricity
0.00057
Inclination
98.815°
RAAN
315.9777°
Arg. of periapsis
324.9927°
True anomaly
124.12384°
Mean anomaly
124.0699°
Eccentric anomaly
124.09687°
Mean motion
3.57077 °/min
Orbital period
100.82 mins
BSTAR
-1.5578e-7
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Other satellites on launch #61 in the year 1993 (1993-09-26 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.STELLA 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-16 02:51:06.685Z | 116.601° SE | 2025-09-16 02:55:06.685Z | 62.828° ENE | 22.928° | 2025-09-16 02:59:06.685Z | 12.264° NNE |
| 8 mins | 2025-09-16 04:31:06.685Z | 201.72° SSW | 2025-09-16 04:34:06.685Z | 253.313° W | 32.449° | 2025-09-16 04:39:06.685Z | 329.991° NNW |
| 9 mins | 2025-09-16 16:45:06.685Z | 17.693° NNE | 2025-09-16 16:49:06.685Z | 86.94° E | 44.344° | 2025-09-16 16:54:06.685Z | 189.898° SSW |
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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