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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 25286.62629509 .00015193 00000-0 50173-3 0 9995
2 56953 97.5934 56.0336 0009828 111.2263 249.0029 15.31449869129786Epoch: 2025-10-13T15:01Z
TLE epoch observation values (Epoch: 2025-10-13T15:01:51.895Z)
Latitude
0.00001°
Longitude
168.141°
Altitude
477.005 km
Speed
7.626 km/s
True Right ascension
03h 44m 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
21:34:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.173 km
Perigee altitude
461.716 km
Semi-major axis
6,846.581 km
Eccentricity
0.00098
Inclination
97.5934°
RAAN
56.0336°
Arg. of periapsis
111.2263°
True anomaly
248.8978°
Mean anomaly
249.0029°
Eccentric anomaly
248.95035°
Mean motion
3.83118 °/min
Orbital period
93.97 mins
BSTAR
0.00050173
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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 | 2025-10-14 08:24:32.373Z | 144.628° SSE | 2025-10-14 08:27:32.373Z | 78.131° E | 34.097° | 2025-10-14 08:30:32.373Z | 3.97° NNE |
| 4 mins | 2025-10-14 21:24:32.373Z | 34.611° NE | 2025-10-14 21:26:32.373Z | 131.876° SE | 37.356° | 2025-10-14 21:28:32.373Z | 174.58° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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