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 55280U 26145.34109435 +.00000000 +00000-0 +79346-4 0 00003
2 55280 69.9991 211.3354 0003573 271.9942 88.0808 14.98340070 04
| Epoch (UTC): | 25 May 2026 08:11:10 |
| Eccentricity: | 0.0003573 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 211.3354° |
| argument of perigee: | 271.9942° |
| revolutions per day: | 14.98340070 |
| mean anomaly at epoch: | 88.0808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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