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 26088.12702769 +.00000000 +00000-0 +68215-4 0 00000
2 05918 81.2332 102.9910 0057553 314.7459 44.9033 14.06300637 07
| Epoch (UTC): | 29 March 2026 03:02:55 |
| Eccentricity: | 0.0057553 |
| inclination: | 81.2332° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 102.9910° |
| argument of perigee: | 314.7459° |
| revolutions per day: | 14.06300637 |
| mean anomaly at epoch: | 44.9033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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