KUIPER-00241, 67149
Orbit data source: Space-Track
KUIPER-00241, 67149 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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67149 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00241
1 67149U 25301S 26171.46240558 .00001291 00000-0 19835-3 0 9991
2 67149 51.9034 341.1810 0000633 108.6340 251.4691 14.79931660 29143Epoch: 2026-06-20T11:05Z
TLE epoch observation values (Epoch: 2026-06-20T11:05:51.842Z)
Latitude
-0.00001°
Longitude
-93.9617°
Altitude
630.428 km
Speed
7.544 km/s
True Right ascension
22h 44m 43s
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
07:12:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.434 km
Perigee altitude
629.547 km
Semi-major axis
7,008.127 km
Eccentricity
0.00006
Inclination
51.9034°
RAAN
341.181°
Arg. of periapsis
108.634°
True anomaly
251.46222°
Mean anomaly
251.4691°
Eccentric anomaly
251.46566°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.00019835
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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-00241 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 21:20:18.660Z | 299.449° NW | 2026-06-20 21:24:18.660Z | 216.929° SW | 40.215° | 2026-06-20 21:28:18.660Z | 145.316° SSE |
| 7 mins | 2026-06-21 13:11:18.660Z | 189.566° SSW | 2026-06-21 13:14:18.660Z | 133.3° SE | 29.118° | 2026-06-21 13:18:18.660Z | 69.193° E |
| 6 mins | 2026-06-21 14:53:18.660Z | 268.948° W | 2026-06-21 14:55:18.660Z | 313.597° NW | 34.939° | 2026-06-21 14:59:18.660Z | 39.988° NE |
| 5 mins | 2026-06-21 16:36:18.660Z | 321.064° NNW | 2026-06-21 16:38:18.660Z | 354.534° N | 18.513° | 2026-06-21 16:41:18.660Z | 36.555° NE |
| 4 mins | 2026-06-21 18:19:18.660Z | 345.215° N | 2026-06-21 18:21:18.660Z | 20.634° NNE | 19.274° | 2026-06-21 18:23:18.660Z | 51.424° ENE |
| 7 mins | 2026-06-21 20:00:18.660Z | 321.805° NNW | 2026-06-21 20:03:18.660Z | 42.451° NE | 38.852° | 2026-06-21 20:07:18.660Z | 109.657° ESE |
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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