RUNNER-1 (TYVAK-1005), 56953
Orbit data source: Space-Track
RUNNER-1 (TYVAK-1005), 56953 is a Chilean 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
CL / CHLERelated 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: 10 hours ago
TLE from 10 hours ago
0 RUNNER-1 (TYVAK-1005)
1 56953U 23084X 26264.12785021 .00007127 00000-0 18448-3 0 9996
2 56953 97.6367 50.0704 0007033 339.6159 20.4804 15.39374749182352Epoch: 2026-09-21T03:04Z
TLE epoch observation values (Epoch: 2026-09-21T03:04:06.258Z)
Latitude
-0.00002°
Longitude
4.0322°
Altitude
446.569 km
Speed
7.647 km/s
True Right ascension
03h 20m 16s
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
06:01:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.706 km
Perigee altitude
440.109 km
Semi-major axis
6,823.044 km
Eccentricity
0.0007
Inclination
97.6367°
RAAN
50.0704°
Arg. of periapsis
339.6159°
True anomaly
20.50862°
Mean anomaly
20.4804°
Eccentric anomaly
20.49451°
Mean motion
3.85102 °/min
Orbital period
93.48 mins
BSTAR
0.00018448
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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 | 2026-09-21 22:21:26.812Z | 33.16° NE | 2026-09-21 22:23:26.812Z | 77.863° E | 38.401° | 2026-09-21 22:26:26.812Z | 166.366° S |
| 4 mins | 2026-09-22 10:24:26.812Z | 210.491° SW | 2026-09-22 10:26:26.812Z | 266.259° W | 30.546° | 2026-09-22 10:28:26.812Z | 316.852° 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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