KUIPER-00177, 67766
Orbit data source: Space-Track
KUIPER-00177, 67766 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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67766 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00177
1 67766U 26030C 26170.85826849 .00000545 00000-0 10055-3 0 9997
2 67766 51.9009 121.3343 0000770 77.7233 282.3816 14.79933498 20300Epoch: 2026-06-19T20:35Z
TLE epoch observation values (Epoch: 2026-06-19T20:35:54.397Z)
Latitude
0.00001°
Longitude
-95.72356°
Altitude
630.165 km
Speed
7.545 km/s
True Right ascension
08h 05m 20s
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
07:21:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.525 km
Perigee altitude
629.445 km
Semi-major axis
7,008.122 km
Eccentricity
0.00008
Inclination
51.9009°
RAAN
121.3343°
Arg. of periapsis
77.7233°
True anomaly
282.37298°
Mean anomaly
282.3816°
Eccentric anomaly
282.37729°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00010055
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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-00177 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-20 22:40:26.700Z | 201.701° SSW | 2026-06-20 22:44:26.700Z | 140.079° SSE | 31.833° | 2026-06-20 22:48:26.700Z | 68.004° E |
| 6 mins | 2026-06-21 00:23:26.700Z | 271.025° WNW | 2026-06-21 00:26:26.700Z | 344.321° N | 33.118° | 2026-06-21 00:29:26.700Z | 37.256° NE |
| 5 mins | 2026-06-21 02:06:26.700Z | 319.056° NNW | 2026-06-21 02:08:26.700Z | 350.733° N | 18.137° | 2026-06-21 02:11:26.700Z | 34.7° NE |
| 5 mins | 2026-06-21 03:49:26.700Z | 341.772° N | 2026-06-21 03:51:26.700Z | 16.838° NNE | 20.151° | 2026-06-21 03:54:26.700Z | 61.3° ENE |
| 7 mins | 2026-06-21 05:30:26.700Z | 318.097° NNW | 2026-06-21 05:33:26.700Z | 30.517° NE | 40.947° | 2026-06-21 05:37:26.700Z | 112.967° SE |
| 5 mins | 2026-06-21 07:12:26.700Z | 269.174° W | 2026-06-21 07:14:26.700Z | 234.741° WSW | 21.915° | 2026-06-21 07:17:26.700Z | 184.682° SSW |
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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