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 56713U 26145.38308376 +.00000000 +00000-0 +10778-3 0 00007
2 56713 87.9172 278.9812 0002310 101.0945 259.0449 13.20771760 08
| Epoch (UTC): | 25 May 2026 09:11:38 |
| Eccentricity: | 0.0002310 |
| inclination: | 87.9172° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9812° |
| argument of perigee: | 101.0945° |
| revolutions per day: | 13.20771760 |
| mean anomaly at epoch: | 259.0449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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