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 55630U 26145.37631441 +.00000000 +00000-0 +44088-4 0 00007
2 55630 69.9998 11.1636 0002541 270.1229 89.9639 14.98331831 09
| Epoch (UTC): | 25 May 2026 09:01:53 |
| Eccentricity: | 0.0002541 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.1636° |
| argument of perigee: | 270.1229° |
| revolutions per day: | 14.98331831 |
| mean anomaly at epoch: | 89.9639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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