TOMORROW-R2, 56962 (Decayed)
Orbit data source: Space-Track
TOMORROW-R2, 56962 was a payload satellite owned by Tomorrow.io (US) in LEO 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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56962 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Astro Digital
Mission
Decayed Commercial Radar Imaging
Bus & Motor
CORVUS-XL, Unknown motor
Mass
85 kg wet, 85 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Dish, 1.0 m
Radar Cross Section
0.425 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 TOMORROW-R2
1 56962U 23084AG 26178.25092823 .08367620 26909-5 30745-3 0 9995
2 56962 97.5928 344.1569 0013162 258.6769 101.3053 16.42951724170684Epoch: 2026-06-27T06:01Z
TLE epoch observation values (Epoch: 2026-06-27T06:01:20.199Z)
Latitude
0.00004°
Longitude
-21.54504°
Altitude
162.909 km
Speed
7.807 km/s
True Right ascension
22h 56m 37s
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
22:01:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.373 km
Perigee altitude
146.176 km
Semi-major axis
6,532.912 km
Eccentricity
0.00132
Inclination
97.5928°
RAAN
344.1569°
Arg. of periapsis
258.6769°
True anomaly
101.45315°
Mean anomaly
101.3053°
Eccentric anomaly
101.37923°
Mean motion
4.11039 °/min
Orbital period
87.58 mins
BSTAR
0.00030745
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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.TOMORROW-R2 Visibility
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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. |
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| This satellite is decayed. |
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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