KUIPER-00101, 65947
Orbit data source: Space-Track
KUIPER-00101, 65947 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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65947 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: 23 hours ago
TLE from 23 hours ago
0 KUIPER-00101
1 65947U 25228A 26277.02488268 -.00000331 00000-0 -14442-4 0 9990
2 65947 51.8981 159.2783 0001221 83.0534 277.0567 14.79920557 54089Epoch: 2026-10-04T00:35Z
TLE epoch observation values (Epoch: 2026-10-04T00:35:49.863Z)
Latitude
-0.00004°
Longitude
137.59645°
Altitude
630.216 km
Speed
7.545 km/s
True Right ascension
10h 37m 06s
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
17:51:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.882 km
Perigee altitude
629.171 km
Semi-major axis
7,008.163 km
Eccentricity
0.00012
Inclination
51.8981°
RAAN
159.2783°
Arg. of periapsis
83.0534°
True anomaly
277.04281°
Mean anomaly
277.0567°
Eccentric anomaly
277.04976°
Mean motion
3.69945 °/min
Orbital period
97.31 mins
BSTAR
-0.000014442
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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-00101 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 | 2026-10-05 01:23:56.722Z | 311.669° NW | 2026-10-05 01:27:56.722Z | 52.998° ENE | 72.962° | 2026-10-05 01:31:56.722Z | 121.061° SE |
| 5 mins | 2026-10-05 03:06:56.722Z | 262.421° W | 2026-10-05 03:08:56.722Z | 230.565° WSW | 18.813° | 2026-10-05 03:11:56.722Z | 188.611° SSW |
| 4 mins | 2026-10-05 17:16:56.722Z | 146.335° SSE | 2026-10-05 17:17:56.722Z | 130.731° SE | 16.854° | 2026-10-05 17:20:56.722Z | 88.605° E |
| 7 mins | 2026-10-05 18:55:56.722Z | 236.68° WSW | 2026-10-05 18:58:56.722Z | 282.975° WNW | 77.53° | 2026-10-05 19:02:56.722Z | 49.833° ENE |
| 6 mins | 2026-10-05 20:38:56.722Z | 302.345° NW | 2026-10-05 20:40:56.722Z | 337.217° NNW | 24.273° | 2026-10-05 20:44:56.722Z | 37.291° NE |
| 5 mins | 2026-10-05 22:21:56.722Z | 333.214° NNW | 2026-10-05 22:23:56.722Z | 4.294° NNE | 18.267° | 2026-10-05 22:26:56.722Z | 46.492° ENE |
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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