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: 8 hours ago
TLE from 8 hours ago
0 TOMORROW-R2
1 56962U 23084AG 25350.94125625 .00048083 00000-0 62138-3 0 9990
2 56962 97.5858 132.9285 0005717 202.4461 157.6546 15.58794714140359Epoch: 2025-12-16T22:35Z
TLE epoch observation values (Epoch: 2025-12-16T22:35:24.539Z)
Latitude
0.00002°
Longitude
68.258°
Altitude
397.862 km
Speed
7.67 km/s
True Right ascension
08h 51m 42s
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
04:56:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
391.935 km
Perigee altitude
384.198 km
Semi-major axis
6,766.203 km
Eccentricity
0.00057
Inclination
97.5858°
RAAN
132.9285°
Arg. of periapsis
202.4461°
True anomaly
157.67949°
Mean anomaly
157.6546°
Eccentric anomaly
157.66705°
Mean motion
3.89965 °/min
Orbital period
92.32 mins
BSTAR
0.00062138
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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)
Did you know?
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 | 2025-12-17 09:30:37.031Z | 153.063° SSE | 2025-12-17 09:32:37.031Z | 107.967° ESE | 39.102° | 2025-12-17 09:35:37.031Z | 356.734° N |
| 4 mins | 2025-12-17 22:16:37.031Z | 40.527° NE | 2025-12-17 22:17:37.031Z | 76.031° E | 34.071° | 2025-12-17 22:20:37.031Z | 173.507° 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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