STARLINK-37018, 68103
Orbit data source: Space-Track
STARLINK-37018, 68103 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sun, 08 Mar 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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68103 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: 13 hours ago
TLE from 13 hours ago
0 STARLINK-37018
1 68103U 26044C 26119.35271108 .00033758 00000-0 10426-2 0 9991
2 68103 97.2854 80.2874 0000858 110.5557 249.5778 15.33466578 9345Epoch: 2026-04-29T08:27Z
TLE epoch observation values (Epoch: 2026-04-29T08:27:54.237Z)
Latitude
-0°
Longitude
95.99652°
Altitude
468.796 km
Speed
7.632 km/s
True Right ascension
05h 21m 08s
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
04:40:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.009 km
Perigee altitude
461.835 km
Semi-major axis
6,840.559 km
Eccentricity
0.00009
Inclination
97.2854°
RAAN
80.2874°
Arg. of periapsis
110.5557°
True anomaly
249.56859°
Mean anomaly
249.5778°
Eccentric anomaly
249.57319°
Mean motion
3.83624 °/min
Orbital period
93.84 mins
BSTAR
0.0010426
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Other satellites on launch #44 in the year 2026 (2026-03-08 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-37018 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 | 2026-04-29 21:09:16.015Z | 125.725° SE | 2026-04-29 21:10:16.015Z | 78.303° E | 37.038° | 2026-04-29 21:13:16.015Z | 1.316° NNE |
| 4 mins | 2026-04-30 10:06:16.015Z | 26.325° NE | 2026-04-30 10:08:16.015Z | 145.064° SSE | 40.373° | 2026-04-30 10:10:16.015Z | 181.004° SSW |
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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