KUIPER-00178, 67767
Orbit data source: Space-Track
KUIPER-00178, 67767 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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67767 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-00178
1 67767U 26030D 26171.41668980 -.00009483 00000-0 -12144-2 0 9993
2 67767 51.8989 118.8472 0001213 98.2597 179.2170 14.80010535 5091Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-51.43615°
Longitude
-17.81155°
Altitude
647.849 km
Speed
7.533 km/s
True Right ascension
02h 43m 18s
True Declination
-51° 15' 57"
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
07:21:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.592 km
Perigee altitude
628.892 km
Semi-major axis
7,007.879 km
Eccentricity
0.00012
Inclination
51.8989°
RAAN
118.8472°
Arg. of periapsis
98.2597°
True anomaly
179.21719°
Mean anomaly
179.217°
Eccentric anomaly
179.21709°
Mean motion
3.69967 °/min
Orbital period
97.31 mins
BSTAR
-0.0012144
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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-00178 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 21:52:30.184Z | 150.279° SSE | 2026-06-20 21:54:30.184Z | 120.853° SE | 14.628° | 2026-06-20 21:56:30.184Z | 93.875° ESE |
| 7 mins | 2026-06-20 23:32:30.184Z | 233.387° WSW | 2026-06-20 23:35:30.184Z | 41.874° NE | 43.699° | 2026-06-20 23:39:30.184Z | 51.828° ENE |
| 6 mins | 2026-06-21 01:14:30.184Z | 296.651° NW | 2026-06-21 01:17:30.184Z | 351.319° N | 22.736° | 2026-06-21 01:20:30.184Z | 34.976° NE |
| 4 mins | 2026-06-21 02:58:30.184Z | 342.445° N | 2026-06-21 02:59:30.184Z | 358.711° N | 17.203° | 2026-06-21 03:02:30.184Z | 42.829° NE |
| 6 mins | 2026-06-21 04:39:30.184Z | 330.239° NNW | 2026-06-21 04:42:30.184Z | 28.77° NE | 27.745° | 2026-06-21 04:45:30.184Z | 81.327° E |
| 7 mins | 2026-06-21 06:21:30.184Z | 294.055° NW | 2026-06-21 06:24:30.184Z | 192.728° SSW | 39.703° | 2026-06-21 06:28:30.184Z | 143.212° SSE |
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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