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: 5 hours ago
TLE from 5 hours ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 26166.11501017 .00009040 00000-0 24641-3 0 9995
2 56953 97.6232 308.1353 0007000 328.0208 32.0611 15.37692753167287Epoch: 2026-06-15T02:45Z
TLE epoch observation values (Epoch: 2026-06-15T02:45:36.878Z)
Latitude
0.00002°
Longitude
3.3256°
Altitude
451.989 km
Speed
7.643 km/s
True Right ascension
20h 32m 32s
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
18:21:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
454.665 km
Perigee altitude
445.106 km
Semi-major axis
6,828.023 km
Eccentricity
0.0007
Inclination
97.6232°
RAAN
308.1353°
Arg. of periapsis
328.0208°
True anomaly
32.10371°
Mean anomaly
32.0611°
Eccentric anomaly
32.0824°
Mean motion
3.84681 °/min
Orbital period
93.58 mins
BSTAR
0.00024641
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-15 09:08:50.066Z | 138.601° SSE | 2026-06-15 09:10:50.066Z | 91.489° ESE | 32.236° | 2026-06-15 09:13:50.066Z | 6.255° NNE |
| 5 mins | 2026-06-15 22:04:50.066Z | 36.665° NE | 2026-06-15 22:06:50.066Z | 113.801° SE | 35.597° | 2026-06-15 22:09:50.066Z | 174.721° S |
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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