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: 2 days ago
TLE from 2 days ago
0 TOMORROW-S2
1 60485U 24149T 25312.65409399 .00012428 00000-0 45392-3 0 9994
2 60485 97.4026 29.5880 0002482 357.2389 2.8837 15.28249646 68355Epoch: 2025-11-08T15:41Z
TLE epoch observation values (Epoch: 2025-11-08T15:41:53.720Z)
Latitude
0.00001°
Longitude
106.03356°
Altitude
482.446 km
Speed
7.625 km/s
True Right ascension
01h 58m 21s
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
15:30:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
479.701 km
Perigee altitude
476.298 km
Semi-major axis
6,856.136 km
Eccentricity
0.00025
Inclination
97.4026°
RAAN
29.588°
Arg. of periapsis
357.2389°
True anomaly
2.88513°
Mean anomaly
2.8837°
Eccentric anomaly
2.88442°
Mean motion
3.82317 °/min
Orbital period
94.16 mins
BSTAR
0.00045392
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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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 | 2025-11-11 05:06:16.480Z | 155.363° SSE | 2025-11-11 05:09:16.480Z | 107.361° ESE | 39.641° | 2025-11-11 05:12:16.480Z | 358.514° N |
| 6 mins | 2025-11-11 18:07:16.480Z | 13.662° NNE | 2025-11-11 18:10:16.480Z | 182.355° SSW | 42.174° | 2025-11-11 18:13:16.480Z | 191.356° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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