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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: 12 hours ago

TLE from 12 hours ago
0 TOMORROW-R2
1 56962U 23084AG  26079.95721319  .00109762  00000-0  76308-3 0  9998
2 56962  97.5904 234.2351 0005195 214.3897 145.7031 15.74058039155068
Epoch: 2026-03-20T22:58Z
TLE epoch observation values (Epoch: 2026-03-20T22:58:23.219Z)
Latitude
-0.00005°
Longitude
71.15353°
Altitude
353.358 km
Speed
7.695 km/s
True Right ascension
15h 36m 56s
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
16:20:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
347.708 km
Perigee altitude
340.723 km
Semi-major axis
6,722.352 km
Eccentricity
0.00052
Inclination
97.5904°
RAAN
234.2351°
Arg. of periapsis
214.3897°
True anomaly
145.73663°
Mean anomaly
145.7031°
Eccentric anomaly
145.71986°
Mean motion
3.93787 °/min
Orbital period
91.42 mins
BSTAR
0.00076308
Loading maneuver chart data...
Computing Atmospheric mass density...

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