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 13594U 26088.21454926 +.00000000 +00000-0 +64727-5 0 00003
2 13594 65.0684 157.0260 0048965 1.3957 358.7236 13.93197871 04
| Epoch (UTC): | 29 March 2026 05:08:57 |
| Eccentricity: | 0.0048965 |
| inclination: | 65.0684° |
| perigee height: | 882 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 157.0260° |
| argument of perigee: | 1.3957° |
| revolutions per day: | 13.93197871 |
| mean anomaly at epoch: | 358.7236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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