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 57718U 26145.41629201 +.00000000 +00000-0 +17383-4 0 00000
2 57718 43.0059 44.8610 0000865 272.2140 87.8613 15.27579226 00
| Epoch (UTC): | 25 May 2026 09:59:27 |
| Eccentricity: | 0.0000865 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.8610° |
| argument of perigee: | 272.2140° |
| revolutions per day: | 15.27579226 |
| mean anomaly at epoch: | 87.8613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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