TOMORROW-R2, 56962
Orbit data source: Space-Track
TOMORROW-R2, 56962 is a payload satellite owned by Tomorrow.io (US) 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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56962 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Astro Digital
Mission
Operational 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: 1 day ago
TLE from 1 day ago
0 TOMORROW-R2
1 56962U 23084AG 25306.37712426 .00044975 00000-0 70794-3 0 9992
2 56962 97.5860 85.5958 0005755 12.3342 347.8050 15.53449002133425Epoch: 2025-11-02T09:03Z
TLE epoch observation values (Epoch: 2025-11-02T09:03:03.536Z)
Latitude
-0.00005°
Longitude
-92.06265°
Altitude
405.978 km
Speed
7.669 km/s
True Right ascension
05h 42m 22s
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
15:50:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
407.497 km
Perigee altitude
399.691 km
Semi-major axis
6,781.731 km
Eccentricity
0.00058
Inclination
97.586°
RAAN
85.5958°
Arg. of periapsis
12.3342°
True anomaly
347.79106°
Mean anomaly
347.805°
Eccentric anomaly
347.79803°
Mean motion
3.88626 °/min
Orbital period
92.63 mins
BSTAR
0.00070794
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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 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 | 2025-11-03 22:42:04.777Z | 353.648° N | 2025-11-03 22:45:04.777Z | 271.815° WNW | 30.266° | 2025-11-03 22:47:04.777Z | 222.707° SW |
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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