KUIPER-00275, 67793
Orbit data source: Space-Track
KUIPER-00275, 67793 is a payload satellite owned by Kuiper Systems (FR) in LEO that was launched on Thu, 12 Feb 2026 UTC via an ARIANE 64 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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67793 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 KUIPER-00275
1 67793U 26030AF 26052.83335647 -.00012850 00000-0 -37097-3 0 9994
2 67793 51.8842 295.6403 0007952 8.3775 65.9588 15.34226987 1306Epoch: 2026-02-21T20:00Z
TLE epoch observation values (Epoch: 2026-02-21T20:00:01.999Z)
Latitude
49.42687°
Longitude
-90.45481°
Altitude
466.555 km
Speed
7.64 km/s
True Right ascension
00h 05m 12s
True Declination
49° 14' 59"
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
05:27:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.123 km
Perigee altitude
458.241 km
Semi-major axis
6,841.819 km
Eccentricity
0.0008
Inclination
51.8842°
RAAN
295.6403°
Arg. of periapsis
8.3775°
True anomaly
66.04205°
Mean anomaly
65.9588°
Eccentric anomaly
66.00042°
Mean motion
3.83518 °/min
Orbital period
93.87 mins
BSTAR
-0.00037097
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Other satellites on launch #30 in the year 2026 (2026-02-12 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.KUIPER-00275 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-22 02:27:38.423Z | 284.975° WNW | 2026-02-22 02:30:38.423Z | 207.134° SW | 28.172° | 2026-02-22 02:32:38.423Z | 165.977° S |
| 5 mins | 2026-02-22 19:20:38.423Z | 254.242° W | 2026-02-22 19:22:38.423Z | 307.177° NW | 38.177° | 2026-02-22 19:25:38.423Z | 41.264° NE |
| 4 mins | 2026-02-23 00:17:38.423Z | 350.547° N | 2026-02-23 00:18:38.423Z | 17.661° NNE | 25.165° | 2026-02-23 00:21:38.423Z | 84.183° E |
| 5 mins | 2026-02-23 01:54:38.423Z | 286.371° WNW | 2026-02-23 01:56:38.423Z | 230.415° WSW | 34.175° | 2026-02-23 01:59:38.423Z | 154.642° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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