STARLINK-36297, 67671
Orbit data source: Space-Track
STARLINK-36297, 67671 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Mon, 02 Feb 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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67671 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: 16 hours ago
TLE from 16 hours ago
0 STARLINK-36297
1 67671U 26022Z 26095.09080478 .00016368 00000-0 50808-3 0 9995
2 67671 97.2860 129.1307 0001903 133.7785 226.3615 15.33453631 9627Epoch: 2026-04-05T02:10Z
TLE epoch observation values (Epoch: 2026-04-05T02:10:45.532Z)
Latitude
-0.0001°
Longitude
-96.96022°
Altitude
469.529 km
Speed
7.631 km/s
True Right ascension
08h 36m 31s
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
23:40:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.762 km
Perigee altitude
461.159 km
Semi-major axis
6,840.597 km
Eccentricity
0.00019
Inclination
97.286°
RAAN
129.1307°
Arg. of periapsis
133.7785°
True anomaly
226.34572°
Mean anomaly
226.3615°
Eccentric anomaly
226.35361°
Mean motion
3.83621 °/min
Orbital period
93.84 mins
BSTAR
0.00050808
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Other satellites on launch #22 in the year 2026 (2026-02-02 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-36297 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-06 01:48:09.577Z | 138.364° SSE | 2026-04-06 01:51:09.577Z | 69.935° E | 29.869° | 2026-04-06 01:54:09.577Z | 7.044° NNE |
| 4 mins | 2026-04-06 14:47:09.577Z | 43.135° NE | 2026-04-06 14:48:09.577Z | 76.322° E | 34.447° | 2026-04-06 14:51:09.577Z | 169.729° S |
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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