KUIPER-00259, 67786
Orbit data source: Space-Track
KUIPER-00259, 67786 is a payload satellite owned by Kuiper Systems (US) 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
USRelated business
Manufacturer
Kuiper Systems
Mission
Operational Commercial Communications
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.4 m
Radar Cross Section
2.326 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 KUIPER-00259
1 67786U 26030Y 26171.17830977 .00003036 00000-0 42766-3 0 9994
2 67786 51.8989 104.9126 0000016 151.4523 208.6440 14.79876591 20561Epoch: 2026-06-20T04:16Z
TLE epoch observation values (Epoch: 2026-06-20T04:16:45.964Z)
Latitude
-0.00002°
Longitude
132.32441°
Altitude
630.47 km
Speed
7.544 km/s
True Right ascension
06h 59m 39s
True Declination
0° 00' 00"
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
07:18:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.176 km
Perigee altitude
630.154 km
Semi-major axis
7,008.302 km
Eccentricity
0
Inclination
51.8989°
RAAN
104.9126°
Arg. of periapsis
151.4523°
True anomaly
208.64391°
Mean anomaly
208.644°
Eccentric anomaly
208.64396°
Mean motion
3.69934 °/min
Orbital period
97.31 mins
BSTAR
0.00042766
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 22:17:55.734Z | 220.172° SW | 2026-06-20 22:20:55.734Z | 107.746° ESE | 43.324° | 2026-06-20 22:24:55.734Z | 55.833° ENE |
| 6 mins | 2026-06-20 23:59:55.734Z | 290.016° WNW | 2026-06-21 00:02:55.734Z | 348.784° N | 25.247° | 2026-06-21 00:05:55.734Z | 34.704° NE |
| 4 mins | 2026-06-21 01:43:55.734Z | 339.679° N | 2026-06-21 01:44:55.734Z | 355.923° N | 17.129° | 2026-06-21 01:47:55.734Z | 39.661° NE |
| 6 mins | 2026-06-21 03:24:55.734Z | 330.407° NNW | 2026-06-21 03:27:55.734Z | 23.721° NE | 24.899° | 2026-06-21 03:30:55.734Z | 74.01° E |
| 7 mins | 2026-06-21 05:06:55.734Z | 303.318° NW | 2026-06-21 05:09:55.734Z | 180.443° SSW | 44.015° | 2026-06-21 05:13:55.734Z | 134.424° SE |
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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