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 65683U 26145.55011394 +.00000000 +00000-0 +10750-1 0 00001
2 65683 53.1618 348.4940 0000934 34.9985 325.1078 15.31297837 02
| Epoch (UTC): | 25 May 2026 13:12:09 |
| Eccentricity: | 0.0000934 |
| inclination: | 53.1618° |
| perigee height: | 471 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 348.4940° |
| argument of perigee: | 34.9985° |
| revolutions per day: | 15.31297837 |
| mean anomaly at epoch: | 325.1078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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