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: 18 hours ago
TLE from 18 hours ago
0 TOMORROW-R2
1 56962U 23084AG 25256.11319937 .00024994 00000-0 47304-3 0 9998
2 56962 97.5835 32.6460 0007050 189.8131 170.2983 15.48351077125639Epoch: 2025-09-13T02:43Z
TLE epoch observation values (Epoch: 2025-09-13T02:43:00.425Z)
Latitude
0.00003°
Longitude
-0.457°
Altitude
429.399 km
Speed
7.651 km/s
True Right ascension
02h 10m 35s
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
13:40:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
423.277 km
Perigee altitude
413.694 km
Semi-major axis
6,796.622 km
Eccentricity
0.00071
Inclination
97.5835°
RAAN
32.646°
Arg. of periapsis
189.8131°
True anomaly
170.3119°
Mean anomaly
170.2983°
Eccentric anomaly
170.3051°
Mean motion
3.8735 °/min
Orbital period
92.94 mins
BSTAR
0.00047304
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-13 21:52:54.134Z | 20.506° NNE | 2025-09-13 21:55:54.134Z | 95.76° ESE | 40.332° | 2025-09-13 21:58:54.134Z | 180.797° SSW |
| 4 mins | 2025-09-14 09:52:54.134Z | 225.581° WSW | 2025-09-14 09:53:54.134Z | 250.558° W | 21.275° | 2025-09-14 09:56:54.134Z | 318.344° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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