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 65323U 26145.44608072 +.00000000 +00000-0 +52940-3 0 00004
2 65323 53.1593 209.8378 0001134 71.3427 288.7698 15.31717464 04
| Epoch (UTC): | 25 May 2026 10:42:21 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.8378° |
| argument of perigee: | 71.3427° |
| revolutions per day: | 15.31717464 |
| mean anomaly at epoch: | 288.7698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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