STARLINK-36416, 67630
Orbit data source: Space-Track
STARLINK-36416, 67630 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Fri, 30 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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67630 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational spacecraft
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 17.7 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 STARLINK-36416
1 67630U 26020P 26104.25982461 .00007883 00000-0 29566-3 0 9999
2 67630 43.0043 298.8942 0001627 266.3064 93.7601 15.27582439 11557Epoch: 2026-04-14T06:14Z
TLE epoch observation values (Epoch: 2026-04-14T06:14:08.846Z)
Latitude
-0.00006°
Longitude
2.91865°
Altitude
482.891 km
Speed
7.626 km/s
True Right ascension
19h 55m 34s
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
09:39:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.103 km
Perigee altitude
483.87 km
Semi-major axis
6,863.123 km
Eccentricity
0.00016
Inclination
43.0043°
RAAN
298.8942°
Arg. of periapsis
266.3064°
True anomaly
93.7787°
Mean anomaly
93.7601°
Eccentric anomaly
93.7694°
Mean motion
3.81734 °/min
Orbital period
94.31 mins
BSTAR
0.00029566
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Other satellites on launch #20 in the year 2026 (2026-01-30 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-36416 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-15 15:22:41.156Z | 195.91° SSW | 2026-04-15 15:25:41.156Z | 135.832° SSE | 21.334° | 2026-04-15 15:27:41.156Z | 98.477° ESE |
| 6 mins | 2026-04-15 17:01:41.156Z | 252.239° W | 2026-04-15 17:03:41.156Z | 259.224° W | 44.176° | 2026-04-15 17:07:41.156Z | 71.823° E |
| 6 mins | 2026-04-15 18:40:41.156Z | 288.736° WNW | 2026-04-15 18:42:41.156Z | 334.174° NNW | 36.79° | 2026-04-15 18:46:41.156Z | 76.755° E |
| 6 mins | 2026-04-15 20:19:41.156Z | 289.592° WNW | 2026-04-15 20:22:41.156Z | 91.567° ESE | 42.792° | 2026-04-15 20:25:41.156Z | 105.859° ESE |
| 4 mins | 2026-04-15 21:59:41.156Z | 244.946° WSW | 2026-04-15 22:00:41.156Z | 220.503° SW | 23.118° | 2026-04-15 22:03:41.156Z | 159.854° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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