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 26071.62076946 +.00000000 +00000-0 -71730-4 0 00005
2 05918 81.2362 118.9761 0057845 2.0005 358.1383 14.06301437 06
| Epoch (UTC): | 12 March 2026 14:53:54 |
| Eccentricity: | 0.0057845 |
| inclination: | 81.2362° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 118.9761° |
| argument of perigee: | 2.0005° |
| revolutions per day: | 14.06301437 |
| mean anomaly at epoch: | 358.1383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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