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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.

Not visible in the next 10 days
Identifier
56962, 2023-084AG
Orbit
SSO
Country
Flag of USUS
Related 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)
2023-06-12 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 TOMORROW-R2
1 56962U 23084AG  26136.39956308  .00187333  14815-4  65625-3 0  9991
2 56962  97.5923 296.5232 0001866 278.2489  81.8571 15.89257486163987
Epoch: 2026-05-16T09:35Z
TLE epoch observation values (Epoch: 2026-05-16T09:35:22.250Z)
Latitude
-0.00002°
Longitude
-81.43659°
Altitude
307.365 km
Speed
7.724 km/s
True Right ascension
19h 46m 05s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
06:49:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
302.492 km
Perigee altitude
300 km
Semi-major axis
6,679.383 km
Eccentricity
0.00019
Inclination
97.5923°
RAAN
296.5232°
Arg. of periapsis
278.2489°
True anomaly
81.87827°
Mean anomaly
81.8571°
Eccentric anomaly
81.86768°
Mean motion
3.97593 °/min
Orbital period
90.54 mins
BSTAR
0.00065625
Loading maneuver chart data...
Computing Atmospheric mass density...

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