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: 11 hours ago
TLE from 11 hours ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 26217.37857812 .00007609 00000-0 20157-3 0 9994
2 56953 97.6299 1.3946 0008877 132.3527 227.8471 15.38622897175160Epoch: 2026-08-05T09:05Z
TLE epoch observation values (Epoch: 2026-08-05T09:05:09.149Z)
Latitude
0°
Longitude
-88.82736°
Altitude
457.361 km
Speed
7.636 km/s
True Right ascension
00h 05m 34s
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
10:13:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.19 km
Perigee altitude
441.073 km
Semi-major axis
6,825.268 km
Eccentricity
0.00089
Inclination
97.6299°
RAAN
1.3946°
Arg. of periapsis
132.3527°
True anomaly
227.77174°
Mean anomaly
227.8471°
Eccentric anomaly
227.80942°
Mean motion
3.84914 °/min
Orbital period
93.53 mins
BSTAR
0.00020157
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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 | 2026-08-05 22:08:04.076Z | 31.903° NE | 2026-08-05 22:11:04.076Z | 108.129° ESE | 30.462° | 2026-08-05 22:13:04.076Z | 159.978° S |
| 4 mins | 2026-08-06 10:12:04.076Z | 211.362° SW | 2026-08-06 10:14:04.076Z | 274.015° WNW | 27.926° | 2026-08-06 10:16:04.076Z | 320.779° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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