KUIPER-00247, 67152
Orbit data source: Space-Track
KUIPER-00247, 67152 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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67152 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-00247
1 67152U 25301V 26171.44750774 .00002743 00000-0 38862-3 0 9993
2 67152 51.8980 323.6973 0000502 119.8986 240.2027 14.79937657 29057Epoch: 2026-06-20T10:44Z
TLE epoch observation values (Epoch: 2026-06-20T10:44:24.668Z)
Latitude
0.00003°
Longitude
-106.06746°
Altitude
630.442 km
Speed
7.544 km/s
True Right ascension
21h 34m 47s
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
07:12:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.324 km
Perigee altitude
629.621 km
Semi-major axis
7,008.109 km
Eccentricity
0.00005
Inclination
51.898°
RAAN
323.6973°
Arg. of periapsis
119.8986°
True anomaly
240.19771°
Mean anomaly
240.2027°
Eccentric anomaly
240.2002°
Mean motion
3.69949 °/min
Orbital period
97.31 mins
BSTAR
0.00038862
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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-00247 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 | 2026-06-20 21:01:03.313Z | 281.98° WNW | 2026-06-20 21:05:03.313Z | 220.161° SW | 21.339° | 2026-06-20 21:08:03.313Z | 178.584° S |
| 7 mins | 2026-06-21 12:52:03.313Z | 226.328° WSW | 2026-06-21 12:55:03.313Z | 83.491° E | 44.198° | 2026-06-21 12:59:03.313Z | 53.858° ENE |
| 6 mins | 2026-06-21 14:34:03.313Z | 292.59° NW | 2026-06-21 14:37:03.313Z | 348.669° N | 24.085° | 2026-06-21 14:40:03.313Z | 34.269° NE |
| 4 mins | 2026-06-21 16:18:03.313Z | 340.133° N | 2026-06-21 16:19:03.313Z | 356.256° N | 17.097° | 2026-06-21 16:22:03.313Z | 40.487° NE |
| 6 mins | 2026-06-21 17:59:03.313Z | 329.843° NNW | 2026-06-21 18:02:03.313Z | 24.519° NE | 26.2° | 2026-06-21 18:05:03.313Z | 76.822° E |
| 7 mins | 2026-06-21 19:41:03.313Z | 299.39° NW | 2026-06-21 19:44:03.313Z | 192.91° SSW | 42.574° | 2026-06-21 19:48:03.313Z | 138.74° SSE |
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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