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 05918U 26067.13847404 +.00000000 +00000-0 -43348-4 0 00005
2 05918 81.2373 123.3159 0058055 14.5029 345.7789 14.06302340 03
| Epoch (UTC): | 08 March 2026 03:19:24 |
| Eccentricity: | 0.0058055 |
| inclination: | 81.2373° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 123.3159° |
| argument of perigee: | 14.5029° |
| revolutions per day: | 14.06302340 |
| mean anomaly at epoch: | 345.7789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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