STARLINK-37105, 68610
Orbit data source: Space-Track
STARLINK-37105, 68610 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sun, 05 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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68610 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, 3.6 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 STARLINK-37105
1 68610U 26073J 26171.29993075 .00019185 00000-0 59466-3 0 9997
2 68610 97.2877 10.6672 0001309 76.4289 283.7100 15.33467931 11616Epoch: 2026-06-20T07:11Z
TLE epoch observation values (Epoch: 2026-06-20T07:11:54.016Z)
Latitude
0.00001°
Longitude
-5.82441°
Altitude
468.375 km
Speed
7.632 km/s
True Right ascension
00h 42m 40s
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
07:16:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.313 km
Perigee altitude
461.522 km
Semi-major axis
6,840.555 km
Eccentricity
0.00013
Inclination
97.2877°
RAAN
10.6672°
Arg. of periapsis
76.4289°
True anomaly
283.69543°
Mean anomaly
283.71°
Eccentric anomaly
283.70271°
Mean motion
3.83624 °/min
Orbital period
93.84 mins
BSTAR
0.00059466
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Other satellites on launch #73 in the year 2026 (2026-04-05 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-37105 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 02:33:04.796Z | 352.882° N | 2026-06-21 02:36:04.796Z | 263.123° W | 32.541° | 2026-06-21 02:38:04.796Z | 219.603° SW |
| 5 mins | 2026-06-21 13:06:04.796Z | 140.911° SSE | 2026-06-21 13:08:04.796Z | 62.805° ENE | 37.391° | 2026-06-21 13:11:04.796Z | 359.673° 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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