KUIPER-00260, 67787
Orbit data source: Space-Track
KUIPER-00260, 67787 is a payload satellite owned by Kuiper Systems (FR) 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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67787 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
Kuiper Systems
Mission
Operational spacecraft
Bus & Motor
KUIPER, Unknown motor
Mass
~490 kg wet, ~490 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 KUIPER-00260
1 67787U 26030Z 26052.83335647 -.00010045 00000-0 -27381-3 0 9996
2 67787 51.8804 295.5337 0001146 84.6153 39.9197 15.35771074 2488Epoch: 2026-02-21T20:00Z
TLE epoch observation values (Epoch: 2026-02-21T20:00:01.999Z)
Latitude
40.52619°
Longitude
-18.06549°
Altitude
461.592 km
Speed
7.641 km/s
True Right ascension
04h 54m 46s
True Declination
40° 20' 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
03:50:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.88 km
Perigee altitude
458.313 km
Semi-major axis
6,837.234 km
Eccentricity
0.00011
Inclination
51.8804°
RAAN
295.5337°
Arg. of periapsis
84.6153°
True anomaly
39.92813°
Mean anomaly
39.9197°
Eccentric anomaly
39.92391°
Mean motion
3.83904 °/min
Orbital period
93.77 mins
BSTAR
-0.00027381
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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-00260 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 | 2026-02-22 02:13:28.133Z | 293.248° NW | 2026-02-22 02:16:28.133Z | 209.379° SW | 35.084° | 2026-02-22 02:19:28.133Z | 150.331° SSE |
| 5 mins | 2026-02-22 19:05:28.133Z | 241.159° WSW | 2026-02-22 19:07:28.133Z | 276.015° WNW | 42.06° | 2026-02-22 19:10:28.133Z | 46.912° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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