LOPEN, 60473
Orbit data source: Space-Track
LOPEN, 60473 is an American payload satellite 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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60473 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ARRAY
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
1.83 kg wet, 1.83 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LOPEN
1 60473U 24149F 25289.16883880 .00015824 00000-0 52850-3 0 9991
2 60473 97.4013 6.8294 0002661 68.4897 291.6627 15.31111599 64810Epoch: 2025-10-16T04:03Z
TLE epoch observation values (Epoch: 2025-10-16T04:03:07.672Z)
Latitude
-0.00008°
Longitude
-78.88498°
Altitude
474.927 km
Speed
7.629 km/s
True Right ascension
00h 27m 19s
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
12:32:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.268 km
Perigee altitude
467.623 km
Semi-major axis
6,847.582 km
Eccentricity
0.00027
Inclination
97.4013°
RAAN
6.8294°
Arg. of periapsis
68.4897°
True anomaly
291.63436°
Mean anomaly
291.6627°
Eccentric anomaly
291.64853°
Mean motion
3.83034 °/min
Orbital period
93.99 mins
BSTAR
0.0005285
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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.LOPEN 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 | 2025-10-16 18:43:08.639Z | 349.577° N | 2025-10-16 18:46:08.639Z | 287.891° WNW | 26.74° | 2025-10-16 18:49:08.639Z | 226.016° WSW |
| 5 mins | 2025-10-17 05:17:08.639Z | 161.953° S | 2025-10-17 05:19:08.639Z | 132.722° SE | 43.56° | 2025-10-17 05:22:08.639Z | 351.253° N |
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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