KUIPER-00226, 67785
Orbit data source: Space-Track
KUIPER-00226, 67785 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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67785 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: 5 hours ago
TLE from 5 hours ago
0 KUIPER-00226
1 67785U 26030X 26052.83335647 -.00014207 00000-0 -44240-3 0 9991
2 67785 51.8812 295.7823 0019282 24.5029 337.3521 15.31770890 1309Epoch: 2026-02-21T20:00Z
TLE epoch observation values (Epoch: 2026-02-21T20:00:01.999Z)
Latitude
1.32282°
Longitude
-154.94388°
Altitude
458.946 km
Speed
7.645 km/s
True Right ascension
19h 47m 15s
True Declination
1° 18' 52"
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
03:54:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.2 km
Perigee altitude
457.787 km
Semi-major axis
6,849.13 km
Eccentricity
0.00193
Inclination
51.8812°
RAAN
295.7823°
Arg. of periapsis
24.5029°
True anomaly
337.26683°
Mean anomaly
337.3521°
Eccentric anomaly
337.30948°
Mean motion
3.82904 °/min
Orbital period
94.02 mins
BSTAR
-0.0004424
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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-00226 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-22 01:09:57.783Z | 322.498° NNW | 2026-02-22 01:12:57.783Z | 50.526° ENE | 34.769° | 2026-02-22 01:15:57.783Z | 105.959° ESE |
| 4 mins | 2026-02-22 02:48:57.783Z | 260.544° W | 2026-02-22 02:49:57.783Z | 238.269° WSW | 20.79° | 2026-02-22 02:52:57.783Z | 178.333° S |
| 4 mins | 2026-02-22 18:05:57.783Z | 168.022° S | 2026-02-22 18:06:57.783Z | 139.968° SSE | 25.257° | 2026-02-22 18:09:57.783Z | 75.411° E |
| 5 mins | 2026-02-22 19:42:57.783Z | 272.975° WNW | 2026-02-22 19:44:57.783Z | 329.082° NNW | 30.755° | 2026-02-22 19:47:57.783Z | 36.7° NE |
| 5 mins | 2026-02-23 00:39:57.783Z | 338.975° N | 2026-02-23 00:41:57.783Z | 50.577° ENE | 31.39° | 2026-02-23 00:44:57.783Z | 101.711° ESE |
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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