STARLINK-37306, 68680
Orbit data source: Space-Track
STARLINK-37306, 68680 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sat, 11 Apr 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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68680 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, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 STARLINK-37306
1 68680U 26077U 26171.21194375 .00014970 00000-0 46489-3 0 9994
2 68680 97.2865 42.4733 0001197 94.9385 265.1995 15.33460147 10873Epoch: 2026-06-20T05:05Z
TLE epoch observation values (Epoch: 2026-06-20T05:05:11.939Z)
Latitude
0°
Longitude
57.74374°
Altitude
468.679 km
Speed
7.632 km/s
True Right ascension
02h 49m 53s
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
08:32:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.26 km
Perigee altitude
461.622 km
Semi-major axis
6,840.578 km
Eccentricity
0.00012
Inclination
97.2865°
RAAN
42.4733°
Arg. of periapsis
94.9385°
True anomaly
265.18583°
Mean anomaly
265.1995°
Eccentric anomaly
265.19267°
Mean motion
3.83622 °/min
Orbital period
93.84 mins
BSTAR
0.00046489
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Other satellites on launch #77 in the year 2026 (2026-04-11 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-37306 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 | 2026-06-21 03:34:56.435Z | 45.175° ENE | 2026-06-21 03:37:56.435Z | 107.664° ESE | 19.758° | 2026-06-21 03:39:56.435Z | 144.863° SSE |
| 5 mins | 2026-06-21 15:40:56.435Z | 184.68° SSW | 2026-06-21 15:42:56.435Z | 273.687° WNW | 41.339° | 2026-06-21 15:45:56.435Z | 340.559° N |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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