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 55289U 26145.37422860 +.00000000 +00000-0 -10984-4 0 00009
2 55289 69.9990 191.1912 0003572 266.9464 93.1287 14.98330687 00
| Epoch (UTC): | 25 May 2026 08:58:53 |
| Eccentricity: | 0.0003572 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 191.1912° |
| argument of perigee: | 266.9464° |
| revolutions per day: | 14.98330687 |
| mean anomaly at epoch: | 93.1287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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