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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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: 7 hours ago
TLE from 7 hours ago
0 TOMORROW-S2
1 60485U 24149T 26046.45673645 .00010119 00000-0 34795-3 0 9994
2 60485 97.3908 127.8504 0002491 8.6621 351.4662 15.30278172 83450Epoch: 2026-02-15T10:57Z
TLE epoch observation values (Epoch: 2026-02-15T10:57:42.029Z)
Latitude
-0.00004°
Longitude
177.96011°
Altitude
476.398 km
Speed
7.628 km/s
True Right ascension
08h 31m 24s
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
20:26:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.64 km
Perigee altitude
470.227 km
Semi-major axis
6,850.07 km
Eccentricity
0.00025
Inclination
97.3908°
RAAN
127.8504°
Arg. of periapsis
8.6621°
True anomaly
351.46196°
Mean anomaly
351.4662°
Eccentric anomaly
351.46408°
Mean motion
3.82825 °/min
Orbital period
94.04 mins
BSTAR
0.00034795
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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 | 2026-02-15 17:47:49.209Z | 27.817° NE | 2026-02-15 17:50:49.209Z | 87.104° E | 32.434° | 2026-02-15 17:53:49.209Z | 166.257° S |
| 5 mins | 2026-02-16 05:55:49.209Z | 210.637° SW | 2026-02-16 05:57:49.209Z | 261.439° W | 26.771° | 2026-02-16 06:00:49.209Z | 324.918° NNW |
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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