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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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, 0.089 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LOPEN
1 60473U 24149F 26311.96869401 .00026221 00000-0 58230-3 0 9990
2 60473 97.3707 36.7896 0002746 96.4710 263.6851 15.43676611124413Epoch: 2026-11-07T23:14Z
TLE epoch observation values (Epoch: 2026-11-07T23:14:55.162Z)
Latitude
0°
Longitude
0.89342°
Altitude
438.599 km
Speed
7.649 km/s
True Right ascension
02h 27m 09s
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
23:36:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.072 km
Perigee altitude
430.332 km
Semi-major axis
6,810.339 km
Eccentricity
0.00027
Inclination
97.3707°
RAAN
36.7896°
Arg. of periapsis
96.471°
True anomaly
263.65383°
Mean anomaly
263.6851°
Eccentric anomaly
263.66946°
Mean motion
3.8618 °/min
Orbital period
93.22 mins
BSTAR
0.0005823
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-09 06:30:28.807Z | 226.314° WSW | 2026-11-09 06:31:28.807Z | 251.742° W | 23.904° | 2026-11-09 06:34:28.807Z | 319.117° NNW |
| 4 mins | 2026-11-09 19:22:28.807Z | 329.66° NNW | 2026-11-09 19:24:28.807Z | 279.025° WNW | 22.655° | 2026-11-09 19:26:28.807Z | 238.45° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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