View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 65924U 26145.45003399 +.00000000 +00000-0 +37807-3 0 00008
2 65924 53.1593 168.9064 0001348 74.7556 285.3594 15.30194096 02
| Epoch (UTC): | 25 May 2026 10:48:02 |
| Eccentricity: | 0.0001348 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9064° |
| argument of perigee: | 74.7556° |
| revolutions per day: | 15.30194096 |
| mean anomaly at epoch: | 285.3594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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