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 56700U 26145.41524578 +.00000000 +00000-0 +15266-3 0 00008
2 56700 43.0029 197.8102 0002043 272.2917 87.7701 15.27578406 00
| Epoch (UTC): | 25 May 2026 09:57:57 |
| Eccentricity: | 0.0002043 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.8102° |
| argument of perigee: | 272.2917° |
| revolutions per day: | 15.27578406 |
| mean anomaly at epoch: | 87.7701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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