KUIPER-00196, 67144
Orbit data source: Space-Track
KUIPER-00196, 67144 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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67144 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-00196
1 67144U 25301M 26171.41668980 -.00042327 00000-0 -54118-2 0 9993
2 67144 51.8978 294.7502 0001321 97.6164 236.1204 14.81047384 5600Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:01.998Z)
Latitude
-20.56373°
Longitude
-140.90258°
Altitude
632.133 km
Speed
7.542 km/s
True Right ascension
18h 30m 56s
True Declination
-20° 26' 56"
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
07:17:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.397 km
Perigee altitude
625.546 km
Semi-major axis
7,004.609 km
Eccentricity
0.00013
Inclination
51.8978°
RAAN
294.7502°
Arg. of periapsis
97.6164°
True anomaly
236.10783°
Mean anomaly
236.1204°
Eccentric anomaly
236.11412°
Mean motion
3.70226 °/min
Orbital period
97.24 mins
BSTAR
-0.0054118
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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-00196 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 10:34:50.794Z | 211.789° SW | 2026-06-21 10:37:50.794Z | 164.874° S | 38.552° | 2026-06-21 10:41:50.794Z | 62.443° ENE |
| 7 mins | 2026-06-21 12:16:50.794Z | 277.777° WNW | 2026-06-21 12:19:50.794Z | 332.598° NNW | 28.418° | 2026-06-21 12:23:50.794Z | 38.702° NE |
| 4 mins | 2026-06-21 14:00:50.794Z | 330.805° NNW | 2026-06-21 14:02:50.794Z | 3.422° NNE | 17.079° | 2026-06-21 14:04:50.794Z | 32.593° NE |
| 5 mins | 2026-06-21 15:42:50.794Z | 337.756° N | 2026-06-21 15:44:50.794Z | 12.925° NNE | 22.414° | 2026-06-21 15:47:50.794Z | 64.58° ENE |
| 7 mins | 2026-06-21 17:23:50.794Z | 310.202° NW | 2026-06-21 17:26:50.794Z | 354.374° N | 44.535° | 2026-06-21 17:30:50.794Z | 125.147° 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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