STARLINK-36704, 67697
Orbit data source: Space-Track
STARLINK-36704, 67697 is a payload satellite owned by SpaceX/Seattle (US) in SSO that was launched on Sat, 07 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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67697 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: 15 hours ago
TLE from 15 hours ago
0 STARLINK-36704
1 67697U 26025E 26103.73520309 .00017665 00000-0 54854-3 0 9995
2 67697 97.2820 215.9281 0000344 36.7311 323.3955 15.33426971 11389Epoch: 2026-04-13T17:38Z
TLE epoch observation values (Epoch: 2026-04-13T17:38:41.546Z)
Latitude
-0.00008°
Longitude
109.33346°
Altitude
468.52 km
Speed
7.632 km/s
True Right ascension
14h 23m 42s
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
15:06:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.775 km
Perigee altitude
462.304 km
Semi-major axis
6,840.676 km
Eccentricity
0.00003
Inclination
97.282°
RAAN
215.9281°
Arg. of periapsis
36.7311°
True anomaly
323.39315°
Mean anomaly
323.3955°
Eccentric anomaly
323.39432°
Mean motion
3.83614 °/min
Orbital period
93.84 mins
BSTAR
0.00054854
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Other satellites on launch #25 in the year 2026 (2026-02-07 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-36704 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 | 2026-04-14 20:50:55.892Z | 326.463° NNW | 2026-04-14 20:51:55.892Z | 295.981° NW | 27.494° | 2026-04-14 20:54:55.892Z | 225.968° WSW |
| 4 mins | 2026-04-15 07:22:55.892Z | 152.761° SSE | 2026-04-15 07:24:55.892Z | 24.611° NE | 40.616° | 2026-04-15 07:26:55.892Z | 355.316° 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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