KUIPER-00197, 67769
Orbit data source: Space-Track
KUIPER-00197, 67769 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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67769 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00197
1 67769U 26030F 26052.58335648 .00057926 00000-0 16467-2 0 9998
2 67769 51.8834 296.7473 0001332 73.3204 104.6910 15.35600281 1308Epoch: 2026-02-21T14:00Z
TLE epoch observation values (Epoch: 2026-02-21T14:00:01.999Z)
Latitude
1.48442°
Longitude
114.0766°
Altitude
459.952 km
Speed
7.638 km/s
True Right ascension
07h 42m 21s
True Declination
1° 28' 31"
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
02:06:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.514 km
Perigee altitude
458.692 km
Semi-major axis
6,837.74 km
Eccentricity
0.00013
Inclination
51.8834°
RAAN
296.7473°
Arg. of periapsis
73.3204°
True anomaly
104.70576°
Mean anomaly
104.691°
Eccentric anomaly
104.69838°
Mean motion
3.83861 °/min
Orbital period
93.78 mins
BSTAR
0.0016467
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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-00197 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-22 00:38:05.370Z | 348.944° N | 2026-02-22 00:39:05.370Z | 14.787° NNE | 24.277° | 2026-02-22 00:42:05.370Z | 82.345° E |
| 5 mins | 2026-02-22 02:15:05.370Z | 287.633° WNW | 2026-02-22 02:17:05.370Z | 230.916° WSW | 34.914° | 2026-02-22 02:20:05.370Z | 153.135° SSE |
| 5 mins | 2026-02-22 19:07:05.370Z | 244.927° WSW | 2026-02-22 19:09:05.370Z | 354.093° N | 42.797° | 2026-02-22 19:12:05.370Z | 47.948° ENE |
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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