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 51717U 26145.25514825 +.00000000 +00000-0 +12822-3 0 00002
2 51717 53.2139 345.4913 0001459 74.8026 285.3127 15.08833052 04
| Epoch (UTC): | 25 May 2026 06:07:24 |
| Eccentricity: | 0.0001459 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 345.4913° |
| argument of perigee: | 74.8026° |
| revolutions per day: | 15.08833052 |
| mean anomaly at epoch: | 285.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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