KUIPER-00252, 67157
Orbit data source: Space-Track
KUIPER-00252, 67157 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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67157 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: 17 hours ago
TLE from 17 hours ago
0 KUIPER-00252
1 67157U 25301AA 26171.14093527 .00000500 00000-0 94582-4 0 9992
2 67157 51.9029 327.5750 0000644 121.3928 238.7097 14.79931662 28973Epoch: 2026-06-20T03:22Z
TLE epoch observation values (Epoch: 2026-06-20T03:22:56.807Z)
Latitude
-0.00005°
Longitude
8.47844°
Altitude
630.521 km
Speed
7.544 km/s
True Right ascension
21h 50m 17s
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
07:14:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.442 km
Perigee altitude
629.539 km
Semi-major axis
7,008.128 km
Eccentricity
0.00006
Inclination
51.9029°
RAAN
327.575°
Arg. of periapsis
121.3928°
True anomaly
238.70339°
Mean anomaly
238.7097°
Eccentric anomaly
238.70655°
Mean motion
3.69948 °/min
Orbital period
97.31 mins
BSTAR
0.000094582
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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-00252 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 11:57:38.585Z | 171.126° S | 2026-06-21 11:59:38.585Z | 135.05° SSE | 23.396° | 2026-06-21 12:02:38.585Z | 83.065° E |
| 7 mins | 2026-06-21 13:37:38.585Z | 251.604° W | 2026-06-21 13:40:38.585Z | 302.696° NW | 38.942° | 2026-06-21 13:44:38.585Z | 43.087° NE |
| 5 mins | 2026-06-21 15:21:38.585Z | 318.027° NNW | 2026-06-21 15:23:38.585Z | 353.393° N | 19.637° | 2026-06-21 15:26:38.585Z | 35.661° NE |
| 4 mins | 2026-06-21 17:04:38.585Z | 344.558° N | 2026-06-21 17:05:38.585Z | 1.029° NNE | 18.168° | 2026-06-21 17:08:38.585Z | 48.015° ENE |
| 7 mins | 2026-06-21 18:45:38.585Z | 325.839° NNW | 2026-06-21 18:48:38.585Z | 35.825° NE | 34.624° | 2026-06-21 18:52:38.585Z | 101.563° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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