KUIPER-00250, 67155
Orbit data source: Space-Track
KUIPER-00250, 67155 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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67155 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-00250
1 67155U 25301Y 26171.19767434 .00000046 00000-0 35008-4 0 9993
2 67155 51.8999 337.3076 0000570 115.6942 244.4079 14.79928435 28873Epoch: 2026-06-20T04:44Z
TLE epoch observation values (Epoch: 2026-06-20T04:44:39.062Z)
Latitude
-0.00006°
Longitude
-2.27096°
Altitude
630.469 km
Speed
7.544 km/s
True Right ascension
22h 29m 13s
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
08:32:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.401 km
Perigee altitude
629.602 km
Semi-major axis
7,008.138 km
Eccentricity
0.00006
Inclination
51.8999°
RAAN
337.3076°
Arg. of periapsis
115.6942°
True anomaly
244.40201°
Mean anomaly
244.4079°
Eccentric anomaly
244.40495°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.000035008
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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-00250 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 13:19:50.337Z | 211.692° SW | 2026-06-21 13:22:50.337Z | 156.754° SSE | 39.587° | 2026-06-21 13:26:50.337Z | 61.47° ENE |
| 7 mins | 2026-06-21 15:01:50.337Z | 279.084° WNW | 2026-06-21 15:04:50.337Z | 335.305° NNW | 28.323° | 2026-06-21 15:08:50.337Z | 39.185° NE |
| 4 mins | 2026-06-21 16:45:50.337Z | 331.187° NNW | 2026-06-21 16:47:50.337Z | 3.765° NNE | 17.152° | 2026-06-21 16:49:50.337Z | 32.852° NE |
| 6 mins | 2026-06-21 18:27:50.337Z | 337.006° NNW | 2026-06-21 18:29:50.337Z | 11.76° NNE | 22.618° | 2026-06-21 18:33:50.337Z | 73.572° E |
| 7 mins | 2026-06-21 20:08:50.337Z | 309.616° NW | 2026-06-21 20:11:50.337Z | 334.318° NNW | 44.224° | 2026-06-21 20:15:50.337Z | 125.802° SE |
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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