KUIPER-00180, 67768
Orbit data source: Space-Track
KUIPER-00180, 67768 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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67768 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: 2 days ago
TLE from 2 days ago
0 KUIPER-00180
1 67768U 26030E 26170.15460036 .00002552 00000-0 36360-3 0 9991
2 67768 51.8988 119.4357 0000747 76.9150 283.1895 14.79934847 20274Epoch: 2026-06-19T03:42Z
TLE epoch observation values (Epoch: 2026-06-19T03:42:37.471Z)
Latitude
-0.00006°
Longitude
156.39188°
Altitude
630.157 km
Speed
7.545 km/s
True Right ascension
07h 57m 44s
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
10:18:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.505 km
Perigee altitude
629.458 km
Semi-major axis
7,008.118 km
Eccentricity
0.00007
Inclination
51.8988°
RAAN
119.4357°
Arg. of periapsis
76.915°
True anomaly
283.18117°
Mean anomaly
283.1895°
Eccentric anomaly
283.18533°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.0003636
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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-00180 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 23:40:26.026Z | 250.459° W | 2026-06-20 23:44:26.026Z | 340.15° N | 39.426° | 2026-06-20 23:48:26.026Z | 45.353° ENE |
| 5 mins | 2026-06-21 01:24:26.026Z | 313.149° NW | 2026-06-21 01:26:26.026Z | 346.751° N | 19.725° | 2026-06-21 01:29:26.026Z | 32.331° NE |
| 5 mins | 2026-06-21 03:07:26.026Z | 339.475° N | 2026-06-21 03:09:26.026Z | 12.615° NNE | 18.387° | 2026-06-21 03:12:26.026Z | 54.838° ENE |
| 7 mins | 2026-06-21 04:48:26.026Z | 322.995° NNW | 2026-06-21 04:51:26.026Z | 21.925° NNE | 34.739° | 2026-06-21 04:55:26.026Z | 100.148° ESE |
| 6 mins | 2026-06-21 06:30:26.026Z | 280.861° WNW | 2026-06-21 06:33:26.026Z | 214.817° SW | 29.591° | 2026-06-21 06:36:26.026Z | 165.874° S |
| 7 mins | 2026-06-21 22:20:26.026Z | 206.75° SW | 2026-06-21 22:23:26.026Z | 119.37° SE | 38.974° | 2026-06-21 22:27:26.026Z | 60.119° 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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