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 57681U 26145.36724058 +.00000000 +00000-0 +64469-5 0 00007
2 57681 53.1597 210.6341 0001095 81.6805 278.4321 15.31697203 03
| Epoch (UTC): | 25 May 2026 08:48:49 |
| Eccentricity: | 0.0001095 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 210.6341° |
| argument of perigee: | 81.6805° |
| revolutions per day: | 15.31697203 |
| mean anomaly at epoch: | 278.4321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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