KUIPER-00246, 67151
Orbit data source: Space-Track
KUIPER-00246, 67151 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Mon, 15 Dec 2025 UTC via an ATLAS V 551 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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67151 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: 11 hours ago
TLE from 11 hours ago
0 KUIPER-00246
1 67151U 25301U 26171.43672941 .00002818 00000-0 39852-3 0 9993
2 67151 51.9008 333.7632 0000615 105.1080 254.9950 14.79929943 28932Epoch: 2026-06-20T10:28Z
TLE epoch observation values (Epoch: 2026-06-20T10:28:53.421Z)
Latitude
-0.00003°
Longitude
-92.11078°
Altitude
630.404 km
Speed
7.544 km/s
True Right ascension
22h 15m 03s
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
08:33:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.427 km
Perigee altitude
629.565 km
Semi-major axis
7,008.133 km
Eccentricity
0.00006
Inclination
51.9008°
RAAN
333.7632°
Arg. of periapsis
105.108°
True anomaly
254.98819°
Mean anomaly
254.995°
Eccentric anomaly
254.9916°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00039852
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Other satellites on launch #301 in the year 2025 (2025-12-15 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-00246 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 | 2026-06-21 12:34:03.982Z | 184.761° SSW | 2026-06-21 12:37:03.982Z | 132.157° SE | 26.238° | 2026-06-21 12:40:03.982Z | 78.907° E |
| 7 mins | 2026-06-21 14:15:03.982Z | 256.876° W | 2026-06-21 14:18:03.982Z | 312.965° NW | 37.228° | 2026-06-21 14:22:03.982Z | 41.841° NE |
| 5 mins | 2026-06-21 15:59:03.982Z | 320.89° NNW | 2026-06-21 16:01:03.982Z | 355.561° N | 18.962° | 2026-06-21 16:04:03.982Z | 36.864° NE |
| 4 mins | 2026-06-21 17:42:03.982Z | 346.267° N | 2026-06-21 17:43:03.982Z | 3.13° NNE | 18.714° | 2026-06-21 17:46:03.982Z | 50.682° ENE |
| 7 mins | 2026-06-21 19:23:03.982Z | 324.654° NNW | 2026-06-21 19:26:03.982Z | 42.692° NE | 36.612° | 2026-06-21 19:30:03.982Z | 105.92° ESE |
| 6 mins | 2026-06-21 21:05:03.982Z | 271.78° WNW | 2026-06-21 21:07:03.982Z | 229.911° WSW | 27.264° | 2026-06-21 21:11:03.982Z | 166.715° 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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