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 26076.17421598 +.00000000 +00000-0 -45732-4 0 00000
2 05918 81.2349 114.5666 0057681 349.1300 10.8617 14.06300461 06
| Epoch (UTC): | 17 March 2026 04:10:52 |
| Eccentricity: | 0.0057681 |
| inclination: | 81.2349° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 114.5666° |
| argument of perigee: | 349.1300° |
| revolutions per day: | 14.06300461 |
| mean anomaly at epoch: | 10.8617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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