RUNNER-1 (TYVAK-1005), 56953
Orbit data source: Space-Track
RUNNER-1 (TYVAK-1005), 56953 is an American payload satellite in SSO that was launched on Mon, 12 Jun 2023 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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56953 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
TYVAK/IMAG
Mission
Operational Commercial Imaging
Bus & Motor
RUNNER, Unknown motor
Mass
86 kg wet, 86 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.4 m
Radar Cross Section
0.619 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 26099.97112394 .00010402 00000-0 29487-3 0 9997
2 56953 97.6128 239.5949 0008050 189.3539 170.7556 15.36417674157126Epoch: 2026-04-09T23:18Z
TLE epoch observation values (Epoch: 2026-04-09T23:18:25.108Z)
Latitude
0°
Longitude
51.7788°
Altitude
465.251 km
Speed
7.631 km/s
True Right ascension
15h 58m 22s
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
02:55:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.165 km
Perigee altitude
448.166 km
Semi-major axis
6,831.803 km
Eccentricity
0.00081
Inclination
97.6128°
RAAN
239.5949°
Arg. of periapsis
189.3539°
True anomaly
170.7704°
Mean anomaly
170.7556°
Eccentric anomaly
170.763°
Mean motion
3.84362 °/min
Orbital period
93.66 mins
BSTAR
0.00029487
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.RUNNER-1 (TYVAK-1005) 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 | 2026-04-10 21:44:57.570Z | 29.251° NE | 2026-04-10 21:47:57.570Z | 97.203° ESE | 32.032° | 2026-04-10 21:50:57.570Z | 168.164° S |
| 4 mins | 2026-04-11 09:49:57.570Z | 210.355° SW | 2026-04-11 09:51:57.570Z | 265.009° W | 27.23° | 2026-04-11 09:53:57.570Z | 316.158° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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