KUIPER-00149, 65968
Orbit data source: Space-Track
KUIPER-00149, 65968 is a payload satellite owned by Kuiper Systems (US) in LEO that was launched on Tue, 14 Oct 2025 UTC via an FALCON 9 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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65968 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: 9 hours ago
TLE from 9 hours ago
0 KUIPER-00149
1 65968U 25228X 26171.46626262 .00002133 00000-0 30863-3 0 9996
2 65968 51.8998 243.6350 0000463 99.1623 260.9391 14.79936441 38764Epoch: 2026-06-20T11:11Z
TLE epoch observation values (Epoch: 2026-06-20T11:11:25.090Z)
Latitude
-0.00007°
Longitude
167.09992°
Altitude
630.323 km
Speed
7.544 km/s
True Right ascension
16h 14m 32s
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
07:15:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.3 km
Perigee altitude
629.651 km
Semi-major axis
7,008.113 km
Eccentricity
0.00005
Inclination
51.8998°
RAAN
243.635°
Arg. of periapsis
99.1623°
True anomaly
260.93386°
Mean anomaly
260.9391°
Eccentric anomaly
260.93648°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00030863
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Other satellites on launch #228 in the year 2025 (2025-10-14 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-00149 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 06:46:50.418Z | 197.626° SSW | 2026-06-21 06:50:50.418Z | 135.929° SSE | 29.455° | 2026-06-21 06:54:50.418Z | 69.414° E |
| 6 mins | 2026-06-21 08:29:50.418Z | 268.597° W | 2026-06-21 08:31:50.418Z | 310.537° NW | 34.395° | 2026-06-21 08:35:50.418Z | 39.292° NE |
| 5 mins | 2026-06-21 10:12:50.418Z | 319.93° NNW | 2026-06-21 10:14:50.418Z | 352.92° N | 18.501° | 2026-06-21 10:17:50.418Z | 35.743° NE |
| 5 mins | 2026-06-21 11:55:50.418Z | 343.834° N | 2026-06-21 11:57:50.418Z | 19.016° NNE | 19.46° | 2026-06-21 12:00:50.418Z | 61.026° ENE |
| 7 mins | 2026-06-21 13:36:50.418Z | 320.884° NNW | 2026-06-21 13:39:50.418Z | 37.748° NE | 39.243° | 2026-06-21 13:43:50.418Z | 109.875° ESE |
| 5 mins | 2026-06-21 15:18:50.418Z | 269.994° W | 2026-06-21 15:20:50.418Z | 232.655° WSW | 24.112° | 2026-06-21 15:23:50.418Z | 180.355° 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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