KUIPER-00186, 67140
Orbit data source: Space-Track
KUIPER-00186, 67140 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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67140 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: 10 hours ago
TLE from 10 hours ago
0 KUIPER-00186
1 67140U 25301H 26171.42594259 .00000769 00000-0 12986-3 0 9997
2 67140 51.9029 343.8320 0000604 103.8232 256.2797 14.79930412 28770Epoch: 2026-06-20T10:13Z
TLE epoch observation values (Epoch: 2026-06-20T10:13:21.439Z)
Latitude
-0.00008°
Longitude
-78.14813°
Altitude
630.391 km
Speed
7.544 km/s
True Right ascension
22h 55m 19s
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
07:13:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.418 km
Perigee altitude
629.571 km
Semi-major axis
7,008.131 km
Eccentricity
0.00006
Inclination
51.9029°
RAAN
343.832°
Arg. of periapsis
103.8232°
True anomaly
256.27298°
Mean anomaly
256.2797°
Eccentric anomaly
256.27634°
Mean motion
3.69947 °/min
Orbital period
97.31 mins
BSTAR
0.00012986
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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-00186 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 20:25:24.983Z | 318.772° NNW | 2026-06-20 20:29:24.983Z | 51.486° ENE | 36.773° | 2026-06-20 20:33:24.983Z | 107.752° ESE |
| 6 mins | 2026-06-20 22:07:24.983Z | 280.289° WNW | 2026-06-20 22:10:24.983Z | 225.219° WSW | 26.369° | 2026-06-20 22:13:24.983Z | 174.065° S |
| 7 mins | 2026-06-21 13:57:24.983Z | 216.17° SW | 2026-06-21 14:00:24.983Z | 139.742° SSE | 42.396° | 2026-06-21 14:04:24.983Z | 58.073° ENE |
| 6 mins | 2026-06-21 15:39:24.983Z | 284.927° WNW | 2026-06-21 15:42:24.983Z | 342.721° N | 26.638° | 2026-06-21 15:45:24.983Z | 33.105° NE |
| 4 mins | 2026-06-21 17:23:24.983Z | 335.651° NNW | 2026-06-21 17:24:24.983Z | 351.574° N | 17.041° | 2026-06-21 17:27:24.983Z | 36.458° NE |
| 5 mins | 2026-06-21 19:05:24.983Z | 339.985° N | 2026-06-21 19:07:24.983Z | 17.822° NNE | 23.875° | 2026-06-21 19:10:24.983Z | 69.537° E |
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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