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 65459U 26145.33335647 +.00000000 +00000-0 +10395-2 0 00004
2 65459 53.1583 261.9627 0001453 100.3958 174.0884 15.34381999 02
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001453 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 261.9627° |
| argument of perigee: | 100.3958° |
| revolutions per day: | 15.34381999 |
| mean anomaly at epoch: | 174.0884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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