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 55414U 26145.39160397 +.00000000 +00000-0 -61527-4 0 00004
2 55414 69.9992 250.9677 0003549 269.9367 90.1385 14.98326508 06
| Epoch (UTC): | 25 May 2026 09:23:54 |
| Eccentricity: | 0.0003549 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 250.9677° |
| argument of perigee: | 269.9367° |
| revolutions per day: | 14.98326508 |
| mean anomaly at epoch: | 90.1385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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