STARLINK-36484, 67404
Orbit data source: Space-Track
STARLINK-36484, 67404 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Mon, 12 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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67404 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 + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 STARLINK-36484
1 67404U 26005A 26170.97888851 .00014210 00000-0 52458-3 0 9999
2 67404 43.0006 20.0282 0001382 277.6359 82.4335 15.27601080 24341Epoch: 2026-06-19T23:29Z
TLE epoch observation values (Epoch: 2026-06-19T23:29:35.967Z)
Latitude
-0.00005°
Longitude
119.42818°
Altitude
482.637 km
Speed
7.626 km/s
True Right ascension
01h 20m 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
07:12:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.88 km
Perigee altitude
483.983 km
Semi-major axis
6,863.068 km
Eccentricity
0.00014
Inclination
43.0006°
RAAN
20.0282°
Arg. of periapsis
277.6359°
True anomaly
82.4492°
Mean anomaly
82.4335°
Eccentric anomaly
82.44135°
Mean motion
3.81738 °/min
Orbital period
94.31 mins
BSTAR
0.00052458
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Other satellites on launch #5 in the year 2026 (2026-01-12 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-36484 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 20:16:47.816Z | 313.232° NW | 2026-06-20 20:17:47.816Z | 3.738° NNE | 38.163° | 2026-06-20 20:20:47.816Z | 77.259° E |
| 5 mins | 2026-06-20 21:54:47.816Z | 286.037° WNW | 2026-06-20 21:56:47.816Z | 233.94° WSW | 44.706° | 2026-06-20 21:59:47.816Z | 113° SE |
| 4 mins | 2026-06-20 23:33:47.816Z | 249.636° W | 2026-06-20 23:35:47.816Z | 208.202° SW | 18.773° | 2026-06-20 23:37:47.816Z | 172.389° S |
| 4 mins | 2026-06-21 16:30:47.816Z | 182.781° SSW | 2026-06-21 16:31:47.816Z | 156.19° SSE | 25.52° | 2026-06-21 16:34:47.816Z | 91.562° ESE |
| 5 mins | 2026-06-21 18:08:47.816Z | 260.623° W | 2026-06-21 18:10:47.816Z | 343.845° N | 44.331° | 2026-06-21 18:13:47.816Z | 70.075° E |
| 5 mins | 2026-06-21 19:47:47.816Z | 293.026° NW | 2026-06-21 19:49:47.816Z | 350.41° N | 37.889° | 2026-06-21 19:52:47.816Z | 75.793° 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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