KUIPER-00175, 67135
Orbit data source: Space-Track
KUIPER-00175, 67135 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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67135 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-00175
1 67135U 25301C 26171.38029286 .00003749 00000-0 38730-3 0 9995
2 67135 51.8952 317.7666 0000825 64.7635 295.3418 14.92275647 29208Epoch: 2026-06-20T09:07Z
TLE epoch observation values (Epoch: 2026-06-20T09:07:37.303Z)
Latitude
-0.00001°
Longitude
-87.73458°
Altitude
591.346 km
Speed
7.566 km/s
True Right ascension
21h 11m 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
07:15:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.871 km
Perigee altitude
590.721 km
Semi-major axis
6,969.433 km
Eccentricity
0.00008
Inclination
51.8952°
RAAN
317.7666°
Arg. of periapsis
64.7635°
True anomaly
295.33326°
Mean anomaly
295.3418°
Eccentric anomaly
295.33753°
Mean motion
3.73033 °/min
Orbital period
96.51 mins
BSTAR
0.0003873
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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-00175 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 20:57:54.487Z | 260.191° W | 2026-06-20 20:59:54.487Z | 230.152° WSW | 14.462° | 2026-06-20 21:01:54.487Z | 201.484° SSW |
| 7 mins | 2026-06-21 12:38:54.487Z | 236.106° WSW | 2026-06-21 12:41:54.487Z | 322.511° NNW | 44.678° | 2026-06-21 12:45:54.487Z | 50.584° ENE |
| 5 mins | 2026-06-21 14:20:54.487Z | 302.714° NW | 2026-06-21 14:22:54.487Z | 339.113° N | 21.482° | 2026-06-21 14:25:54.487Z | 29.804° NE |
| 6 mins | 2026-06-21 17:43:54.487Z | 331.834° NNW | 2026-06-21 17:46:54.487Z | 34.33° NE | 26.732° | 2026-06-21 17:49:54.487Z | 83.786° E |
| 6 mins | 2026-06-21 19:24:54.487Z | 293.356° NW | 2026-06-21 19:26:54.487Z | 250.94° W | 39.044° | 2026-06-21 19:30:54.487Z | 146.06° SSE |
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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