KUIPER-00279, 67795
Orbit data source: Space-Track
KUIPER-00279, 67795 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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67795 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: 13 hours ago
TLE from 13 hours ago
0 KUIPER-00279
1 67795U 26030AH 26171.41668980 -.00030964 00000-0 -20151-2 0 9999
2 67795 51.8895 85.0518 0008470 53.5242 166.2665 15.07308596 4054Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-30.45212°
Longitude
-126.28879°
Altitude
559.305 km
Speed
7.579 km/s
True Right ascension
19h 29m 24s
True Declination
-30° 17' 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
10:18:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.75 km
Perigee altitude
539.023 km
Semi-major axis
6,923.024 km
Eccentricity
0.00085
Inclination
51.8895°
RAAN
85.0518°
Arg. of periapsis
53.5242°
True anomaly
166.28952°
Mean anomaly
166.2665°
Eccentric anomaly
166.27801°
Mean motion
3.7679 °/min
Orbital period
95.54 mins
BSTAR
-0.0020151
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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-00279 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 | 2026-06-20 23:40:31.693Z | 320.171° NNW | 2026-06-20 23:42:31.693Z | 355.038° N | 16.14° | 2026-06-20 23:44:31.693Z | 26.644° NE |
| 4 mins | 2026-06-21 01:21:31.693Z | 344.503° N | 2026-06-21 01:23:31.693Z | 20.006° NNE | 16.016° | 2026-06-21 01:25:31.693Z | 50.421° ENE |
| 5 mins | 2026-06-21 03:01:31.693Z | 333.851° NNW | 2026-06-21 03:03:31.693Z | 36.088° NE | 34.575° | 2026-06-21 03:06:31.693Z | 99.739° ESE |
| 5 mins | 2026-06-21 04:40:31.693Z | 276.714° WNW | 2026-06-21 04:42:31.693Z | 236.612° WSW | 25.662° | 2026-06-21 04:45:31.693Z | 174.166° S |
| 6 mins | 2026-06-21 20:12:31.693Z | 195.652° SSW | 2026-06-21 20:15:31.693Z | 118.886° SE | 31.422° | 2026-06-21 20:18:31.693Z | 67.916° E |
| 5 mins | 2026-06-21 21:52:31.693Z | 278.286° WNW | 2026-06-21 21:54:31.693Z | 325.882° NNW | 29.912° | 2026-06-21 21:57:31.693Z | 32.849° NE |
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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