KUIPER-00262, 67788
Orbit data source: Space-Track
KUIPER-00262, 67788 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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67788 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: 12 hours ago
TLE from 12 hours ago
0 KUIPER-00262
1 67788U 26030AA 26171.34955634 .00002748 00000-0 39025-3 0 9996
2 67788 51.9002 101.6628 0001025 117.4164 242.6902 14.79830130 20622Epoch: 2026-06-20T08:23Z
TLE epoch observation values (Epoch: 2026-06-20T08:23:21.667Z)
Latitude
-0.00008°
Longitude
67.257°
Altitude
630.937 km
Speed
7.544 km/s
True Right ascension
06h 46m 39s
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
07:15:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.03 km
Perigee altitude
629.593 km
Semi-major axis
7,008.448 km
Eccentricity
0.0001
Inclination
51.9002°
RAAN
101.6628°
Arg. of periapsis
117.4164°
True anomaly
242.67976°
Mean anomaly
242.6902°
Eccentric anomaly
242.68498°
Mean motion
3.69922 °/min
Orbital period
97.32 mins
BSTAR
0.00039025
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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-00262 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 21:30:51.493Z | 195.432° SSW | 2026-06-20 21:33:51.493Z | 142.856° SSE | 31.104° | 2026-06-20 21:37:51.493Z | 69.065° E |
| 7 mins | 2026-06-20 23:12:51.493Z | 269.235° W | 2026-06-20 23:15:51.493Z | 341.011° N | 33.725° | 2026-06-20 23:19:51.493Z | 42.532° NE |
| 5 mins | 2026-06-21 00:55:51.493Z | 317.516° NNW | 2026-06-21 00:57:51.493Z | 348.842° N | 18.21° | 2026-06-21 01:00:51.493Z | 33.572° NE |
| 5 mins | 2026-06-21 02:38:51.493Z | 340.259° N | 2026-06-21 02:40:51.493Z | 14.642° NNE | 20.035° | 2026-06-21 02:43:51.493Z | 59.868° ENE |
| 7 mins | 2026-06-21 04:19:51.493Z | 317.997° NNW | 2026-06-21 04:22:51.493Z | 22.707° NE | 40.427° | 2026-06-21 04:26:51.493Z | 111.709° ESE |
| 6 mins | 2026-06-21 06:01:51.493Z | 271.301° WNW | 2026-06-21 06:03:51.493Z | 237.572° WSW | 22.291° | 2026-06-21 06:07:51.493Z | 176.176° S |
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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