KUIPER-00232, 67148
Orbit data source: Space-Track
KUIPER-00232, 67148 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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67148 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: 16 hours ago
TLE from 16 hours ago
0 KUIPER-00232
1 67148U 25301R 26171.16930942 .00003213 00000-0 45028-3 0 9999
2 67148 51.9006 332.4876 0000601 113.3506 246.7520 14.79935527 28905Epoch: 2026-06-20T04:03Z
TLE epoch observation values (Epoch: 2026-06-20T04:03:48.333Z)
Latitude
-0.00001°
Longitude
3.14841°
Altitude
630.441 km
Speed
7.544 km/s
True Right ascension
22h 09m 57s
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
07:13:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.4 km
Perigee altitude
629.558 km
Semi-major axis
7,008.116 km
Eccentricity
0.00006
Inclination
51.9006°
RAAN
332.4876°
Arg. of periapsis
113.3506°
True anomaly
246.74567°
Mean anomaly
246.752°
Eccentric anomaly
246.74884°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00045028
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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-00232 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 20:47:29.823Z | 297.228° NW | 2026-06-20 20:51:29.823Z | 217.809° SW | 37.889° | 2026-06-20 20:55:29.823Z | 149.292° SSE |
| 7 mins | 2026-06-21 12:38:29.823Z | 193.542° SSW | 2026-06-21 12:41:29.823Z | 132.782° SE | 31.666° | 2026-06-21 12:45:29.823Z | 67.074° ENE |
| 6 mins | 2026-06-21 14:20:29.823Z | 272.915° WNW | 2026-06-21 14:22:29.823Z | 315.842° NNW | 33.168° | 2026-06-21 14:26:29.823Z | 38.802° NE |
| 5 mins | 2026-06-21 16:03:29.823Z | 321.895° NNW | 2026-06-21 16:05:29.823Z | 354.627° N | 18.156° | 2026-06-21 16:08:29.823Z | 36.832° NE |
| 5 mins | 2026-06-21 17:46:29.823Z | 345.034° N | 2026-06-21 17:48:29.823Z | 21.03° NNE | 19.933° | 2026-06-21 17:51:29.823Z | 63.156° ENE |
| 7 mins | 2026-06-21 19:27:29.823Z | 319.527° NNW | 2026-06-21 19:30:29.823Z | 45.512° ENE | 40.615° | 2026-06-21 19:34:29.823Z | 113.232° SE |
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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