DECAYED
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TOMORROW-R1, 56199 (Decayed)

Orbit data source: Space-Track

TOMORROW-R1, 56199 was a payload satellite owned by Tomorrow.io (US) in LEO that was launched on Sat, 15 Apr 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
56199, 2023-054X
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)
2023-04-15 (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: 10 months ago

TLE from 10 months ago
0 TOMORROW-R1
1 56199U 23054X   25106.71816979  .07119911  25345-5  90198-3 0  9999
2 56199  97.3068  18.5542 0005511 219.6712 140.4183 16.36017470113304
Epoch: 2025-04-16T17:14Z
TLE epoch observation values (Epoch: 2025-04-16T17:14:09.869Z)
Latitude
-0.00006°
Longitude
-85.08732°
Altitude
182.452 km
Speed
7.795 km/s
True Right ascension
01h 14m 13s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
00:15:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.837 km
Perigee altitude
169.616 km
Semi-major axis
6,551.364 km
Eccentricity
0.00055
Inclination
97.3068°
RAAN
18.5542°
Arg. of periapsis
219.6712°
True anomaly
140.45852°
Mean anomaly
140.4183°
Eccentric anomaly
140.43841°
Mean motion
4.09304 °/min
Orbital period
87.95 mins
BSTAR
0.00090198
Loading maneuver chart data...
Computing Atmospheric mass density...

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