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: 10 hours ago
TLE from 10 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
07:19:12
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 21:59:27.140Z | 266.284° W | 2026-06-20 22:01:27.140Z | 311.975° NW | 33.815° | 2026-06-20 22:05:27.140Z | 41.115° NE |
| 4 mins | 2026-06-21 01:21:27.140Z | 343.353° N | 2026-06-21 01:23:27.140Z | 18.615° NNE | 16.095° | 2026-06-21 01:25:27.140Z | 49.529° ENE |
| 5 mins | 2026-06-21 03:01:27.140Z | 332.796° NNW | 2026-06-21 03:03:27.140Z | 32.606° NE | 34.631° | 2026-06-21 03:06:27.140Z | 99.227° ESE |
| 5 mins | 2026-06-21 04:40:27.140Z | 277.621° WNW | 2026-06-21 04:42:27.140Z | 238.718° WSW | 25.521° | 2026-06-21 04:45:27.140Z | 174.961° S |
| 6 mins | 2026-06-21 20:12:27.140Z | 196.349° SSW | 2026-06-21 20:15:27.140Z | 121.709° SE | 31.65° | 2026-06-21 20:18:27.140Z | 68.377° 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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