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: 7 hours ago
TLE from 7 hours ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 25334.82433029 .00011559 00000-0 36643-3 0 9999
2 56953 97.5974 105.4679 0007527 306.4128 53.6419 15.32851396137167Epoch: 2025-11-30T19:47Z
TLE epoch observation values (Epoch: 2025-11-30T19:47:02.137Z)
Latitude
0.00002°
Longitude
98.77635°
Altitude
467.359 km
Speed
7.634 km/s
True Right ascension
07h 01m 52s
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
00:21:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.417 km
Perigee altitude
459.117 km
Semi-major axis
6,842.404 km
Eccentricity
0.00075
Inclination
97.5974°
RAAN
105.4679°
Arg. of periapsis
306.4128°
True anomaly
53.7114°
Mean anomaly
53.6419°
Eccentric anomaly
53.67665°
Mean motion
3.83469 °/min
Orbital period
93.88 mins
BSTAR
0.00036643
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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 | 2025-12-01 08:26:53.015Z | 139.226° SSE | 2025-12-01 08:29:53.015Z | 73.816° E | 30.397° | 2025-12-01 08:32:53.015Z | 6.958° NNE |
| 5 mins | 2025-12-01 21:25:53.015Z | 37.864° NE | 2025-12-01 21:27:53.015Z | 108.033° ESE | 34.777° | 2025-12-01 21:30:53.015Z | 172.319° 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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