TOMORROW-S2, 60485
Orbit data source: Space-Track
TOMORROW-S2, 60485 is a payload satellite owned by Tomorrow.io (US) in SSO that was launched on Fri, 16 Aug 2024 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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60485 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Operational Commercial Weather
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.138 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 TOMORROW-S2
1 60485U 24149T 25364.49233974 .00012770 00000-0 45126-3 0 9992
2 60485 97.3984 81.1248 0004121 129.1152 231.0455 15.29319826 76276Epoch: 2025-12-30T11:48Z
TLE epoch observation values (Epoch: 2025-12-30T11:48:58.153Z)
Latitude
-0.00004°
Longitude
164.70766°
Altitude
482.725 km
Speed
7.623 km/s
True Right ascension
05h 24m 29s
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
22:20:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.622 km
Perigee altitude
471.973 km
Semi-major axis
6,852.934 km
Eccentricity
0.00041
Inclination
97.3984°
RAAN
81.1248°
Arg. of periapsis
129.1152°
True anomaly
231.00879°
Mean anomaly
231.0455°
Eccentric anomaly
231.02714°
Mean motion
3.82585 °/min
Orbital period
94.1 mins
BSTAR
0.00045126
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-S2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-31 05:13:04.349Z | 158.922° S | 2025-12-31 05:16:04.349Z | 63.864° ENE | 43.25° | 2025-12-31 05:19:04.349Z | 353.512° N |
| 5 mins | 2025-12-31 18:14:04.349Z | 8.234° NNE | 2025-12-31 18:16:04.349Z | 207.555° SW | 42.281° | 2025-12-31 18:19:04.349Z | 195.279° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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