KUIPER-00204, 67145
Orbit data source: Space-Track
KUIPER-00204, 67145 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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67145 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: 1 day ago
TLE from 1 day ago
0 KUIPER-00204
1 67145U 25301N 26170.78599925 .00002914 00000-0 41140-3 0 9993
2 67145 51.9018 314.1622 0000365 164.5992 195.4982 14.79901106 29241Epoch: 2026-06-19T18:51Z
TLE epoch observation values (Epoch: 2026-06-19T18:51:50.335Z)
Latitude
0.00003°
Longitude
123.19251°
Altitude
630.63 km
Speed
7.544 km/s
True Right ascension
20h 56m 38s
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
07:12:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.343 km
Perigee altitude
629.831 km
Semi-major axis
7,008.224 km
Eccentricity
0.00004
Inclination
51.9018°
RAAN
314.1622°
Arg. of periapsis
164.5992°
True anomaly
195.49708°
Mean anomaly
195.4982°
Eccentric anomaly
195.49764°
Mean motion
3.6994 °/min
Orbital period
97.31 mins
BSTAR
0.0004114
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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-00204 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 | 2026-06-21 11:31:58.910Z | 209.874° SW | 2026-06-21 11:35:58.910Z | 149.541° SSE | 36.697° | 2026-06-21 11:39:58.910Z | 64.312° ENE |
| 7 mins | 2026-06-21 13:14:58.910Z | 275.904° WNW | 2026-06-21 13:17:58.910Z | 337.131° NNW | 30.225° | 2026-06-21 13:21:58.910Z | 40.373° NE |
| 4 mins | 2026-06-21 14:58:58.910Z | 331.55° NNW | 2026-06-21 14:59:58.910Z | 347.643° N | 17.406° | 2026-06-21 15:02:58.910Z | 33.166° NE |
| 5 mins | 2026-06-21 16:40:58.910Z | 338.433° N | 2026-06-21 16:42:58.910Z | 13.156° NNE | 21.603° | 2026-06-21 16:45:58.910Z | 62.601° ENE |
| 7 mins | 2026-06-21 18:21:58.910Z | 312.844° NW | 2026-06-21 18:24:58.910Z | 5.591° NNE | 43.431° | 2026-06-21 18:28:58.910Z | 120.369° SE |
| 4 mins | 2026-06-21 20:04:58.910Z | 253.59° W | 2026-06-21 20:05:58.910Z | 237.114° WSW | 17.753° | 2026-06-21 20:08:58.910Z | 192.256° SSW |
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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