KUIPER-00259, 67786
Orbit data source: Space-Track
KUIPER-00259, 67786 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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67786 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-00259
1 67786U 26030Y 26052.83335647 -.00014136 00000-0 -40758-3 0 9993
2 67786 51.8809 295.6272 0007706 4.3774 74.0726 15.34358892 2629Epoch: 2026-02-21T20:00Z
TLE epoch observation values (Epoch: 2026-02-21T20:00:01.999Z)
Latitude
50.59944°
Longitude
-84.33969°
Altitude
467.2 km
Speed
7.64 km/s
True Right ascension
00h 29m 40s
True Declination
50° 25' 25"
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
03:49:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.563 km
Perigee altitude
458.018 km
Semi-major axis
6,841.428 km
Eccentricity
0.00077
Inclination
51.8809°
RAAN
295.6272°
Arg. of periapsis
4.3774°
True anomaly
74.15754°
Mean anomaly
74.0726°
Eccentric anomaly
74.11507°
Mean motion
3.83551 °/min
Orbital period
93.86 mins
BSTAR
-0.00040758
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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-00259 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 00:48:46.147Z | 329.55° NNW | 2026-02-22 00:50:46.147Z | 10.606° NNE | 27.199° | 2026-02-22 00:53:46.147Z | 87.252° E |
| 5 mins | 2026-02-22 02:26:46.147Z | 282.584° WNW | 2026-02-22 02:28:46.147Z | 234.903° WSW | 29.384° | 2026-02-22 02:31:46.147Z | 162.65° S |
| 5 mins | 2026-02-22 19:19:46.147Z | 256.547° W | 2026-02-22 19:21:46.147Z | 334.572° NNW | 39.121° | 2026-02-22 19:24:46.147Z | 43.514° NE |
| 5 mins | 2026-02-23 00:15:46.147Z | 339.673° N | 2026-02-23 00:17:46.147Z | 30.275° NE | 25.054° | 2026-02-23 00:20:46.147Z | 87.203° E |
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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