RUNNER-1 (TYVAK-1005), 56953
Orbit data source: Space-Track
RUNNER-1 (TYVAK-1005), 56953 is an Israeli 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
IL / ISRARelated 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, 0.6 m
Radar Cross Section
0.619 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 26308.38344032 .00008099 00000-0 20368-3 0 9999
2 56953 97.6417 96.2521 0007784 162.9232 197.2277 15.40205012189160Epoch: 2026-11-04T09:12Z
TLE epoch observation values (Epoch: 2026-11-04T09:12:09.243Z)
Latitude
-0.00001°
Longitude
-85.41895°
Altitude
453.689 km
Speed
7.637 km/s
True Right ascension
06h 25m 00s
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
23:13:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
447.762 km
Perigee altitude
437.144 km
Semi-major axis
6,820.59 km
Eccentricity
0.00078
Inclination
97.6417°
RAAN
96.2521°
Arg. of periapsis
162.9232°
True anomaly
197.20131°
Mean anomaly
197.2277°
Eccentric anomaly
197.2145°
Mean motion
3.8531 °/min
Orbital period
93.43 mins
BSTAR
0.00020368
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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 | 2026-11-06 09:40:39.512Z | 138.704° SSE | 2026-11-06 09:42:39.512Z | 92.818° ESE | 38.672° | 2026-11-06 09:45:39.512Z | 6.597° NNE |
| 4 mins | 2026-11-06 22:35:39.512Z | 41.551° NE | 2026-11-06 22:37:39.512Z | 124.507° SE | 40.625° | 2026-11-06 22:39:39.512Z | 168.411° 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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