DECAYED
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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.

Not visible in the next 10 days
Identifier
56962, 2023-084AG
Orbit
Decayed
Country
Flag of USUS
Related 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)
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: 3 months ago

TLE from 3 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 16.42951724170684
Epoch: 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
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
02:57:35
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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Computing Atmospheric mass density...

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