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 55652U 26145.53463022 +.00000000 +00000-0 +67500-4 0 00001
2 55652 69.9994 350.6377 0002975 267.9683 92.1136 14.98327306 01
| Epoch (UTC): | 25 May 2026 12:49:52 |
| Eccentricity: | 0.0002975 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 350.6377° |
| argument of perigee: | 267.9683° |
| revolutions per day: | 14.98327306 |
| mean anomaly at epoch: | 92.1136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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