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 55393U 26145.49985346 +.00000000 +00000-0 +23801-4 0 00002
2 55393 69.9992 230.6858 0003612 268.4269 91.6477 14.98330613 04
| Epoch (UTC): | 25 May 2026 11:59:47 |
| Eccentricity: | 0.0003612 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 230.6858° |
| argument of perigee: | 268.4269° |
| revolutions per day: | 14.98330613 |
| mean anomaly at epoch: | 91.6477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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