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: 17 hours ago
TLE from 17 hours ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 26062.83543942 .00016010 00000-0 46731-3 0 9991
2 56953 97.6058 201.2218 0007600 335.2619 24.8258 15.35390769151423Epoch: 2026-03-03T20:03Z
TLE epoch observation values (Epoch: 2026-03-03T20:03:01.965Z)
Latitude
-0.00009°
Longitude
98.85483°
Altitude
458.148 km
Speed
7.64 km/s
True Right ascension
13h 24m 53s
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
16:33:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.909 km
Perigee altitude
451.52 km
Semi-major axis
6,834.851 km
Eccentricity
0.00076
Inclination
97.6058°
RAAN
201.2218°
Arg. of periapsis
335.2619°
True anomaly
24.8624°
Mean anomaly
24.8258°
Eccentric anomaly
24.8441°
Mean motion
3.84105 °/min
Orbital period
93.72 mins
BSTAR
0.00046731
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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 | 2026-03-04 21:37:58.861Z | 28.101° NE | 2026-03-04 21:40:58.861Z | 89.201° E | 32.387° | 2026-03-04 21:43:58.861Z | 167.199° S |
| 4 mins | 2026-03-05 09:43:58.861Z | 217.372° SW | 2026-03-05 09:45:58.861Z | 278.453° WNW | 25.882° | 2026-03-05 09:47:58.861Z | 320.302° 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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