STARLINK-36423, 67448
Orbit data source: Space-Track
STARLINK-36423, 67448 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 14 Jan 2026 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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67448 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 STARLINK-36423
1 67448U 26008D 26297.21986429 .00021627 00000-0 79275-3 0 9993
2 67448 42.9986 354.5493 0000955 219.4287 140.6495 15.27595085 44525Epoch: 2026-10-24T05:16Z
TLE epoch observation values (Epoch: 2026-10-24T05:16:36.274Z)
Latitude
-0.00004°
Longitude
-117.23108°
Altitude
483.286 km
Speed
7.625 km/s
True Right ascension
23h 38m 11s
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
03:07:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.605 km
Perigee altitude
484.294 km
Semi-major axis
6,863.086 km
Eccentricity
0.0001
Inclination
42.9986°
RAAN
354.5493°
Arg. of periapsis
219.4287°
True anomaly
140.65644°
Mean anomaly
140.6495°
Eccentric anomaly
140.65297°
Mean motion
3.81737 °/min
Orbital period
94.31 mins
BSTAR
0.00079275
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Other satellites on launch #8 in the year 2026 (2026-01-14 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.STARLINK-36423 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-25 08:12:43.541Z | 252.907° W | 2026-10-25 08:15:43.541Z | 25.42° NE | 84.69° | 2026-10-25 08:18:43.541Z | 71.045° E |
| 5 mins | 2026-10-25 09:52:43.541Z | 292.419° WNW | 2026-10-25 09:54:43.541Z | 354.637° N | 50.735° | 2026-10-25 09:57:43.541Z | 73.427° E |
| 6 mins | 2026-10-25 11:31:43.541Z | 290.359° WNW | 2026-10-25 11:33:43.541Z | 315.524° NNW | 76.408° | 2026-10-25 11:37:43.541Z | 106.222° ESE |
| 5 mins | 2026-10-25 13:10:43.541Z | 256.583° W | 2026-10-25 13:12:43.541Z | 211.311° SW | 25.419° | 2026-10-25 13:15:43.541Z | 157.053° SSE |
| 4 mins | 2026-10-26 06:07:43.541Z | 179.358° S | 2026-10-26 06:08:43.541Z | 157.477° SSE | 23.002° | 2026-10-26 06:11:43.541Z | 96.548° ESE |
| 5 mins | 2026-10-26 07:45:43.541Z | 252.553° W | 2026-10-26 07:47:43.541Z | 275.642° WNW | 84.084° | 2026-10-26 07:50:43.541Z | 71.176° 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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