KUIPER-00270, 67791
Orbit data source: Space-Track
KUIPER-00270, 67791 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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67791 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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00270
1 67791U 26030AD 26171.41668980 -.00054062 00000-0 -45925-2 0 9996
2 67791 51.8947 86.9836 0010521 48.9827 54.1676 14.97528957 4801Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
50.14063°
Longitude
139.24848°
Altitude
575.989 km
Speed
7.581 km/s
True Right ascension
13h 11m 33s
True Declination
49° 58' 01"
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
08:33:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.305 km
Perigee altitude
567.674 km
Semi-major axis
6,953.127 km
Eccentricity
0.00105
Inclination
51.8947°
RAAN
86.9836°
Arg. of periapsis
48.9827°
True anomaly
54.26542°
Mean anomaly
54.1676°
Eccentric anomaly
54.2165°
Mean motion
3.74346 °/min
Orbital period
96.17 mins
BSTAR
-0.0045925
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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-00270 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 22:35:46.160Z | 274.837° WNW | 2026-06-20 22:38:46.160Z | 326.376° NNW | 26.976° | 2026-06-20 22:42:46.160Z | 37.853° NE |
| 4 mins | 2026-06-21 00:18:46.160Z | 329.977° NNW | 2026-06-21 00:20:46.160Z | 3.127° NNE | 15.498° | 2026-06-21 00:22:46.160Z | 32.561° NE |
| 5 mins | 2026-06-21 01:59:46.160Z | 339.93° N | 2026-06-21 02:01:46.160Z | 16.424° NNE | 20.287° | 2026-06-21 02:04:46.160Z | 65.499° ENE |
| 7 mins | 2026-06-21 03:39:46.160Z | 312.963° NW | 2026-06-21 03:42:46.160Z | 60.972° ENE | 43.781° | 2026-06-21 03:46:46.160Z | 122.312° SE |
| 4 mins | 2026-06-21 05:20:46.160Z | 258.811° W | 2026-06-21 05:22:46.160Z | 225.792° WSW | 15.856° | 2026-06-21 05:24:46.160Z | 196.124° SSW |
| 6 mins | 2026-06-21 20:58:46.160Z | 227.696° WSW | 2026-06-21 21:00:46.160Z | 214.628° SW | 43.385° | 2026-06-21 21:04:46.160Z | 53.6° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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