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 26100.22214308 +.00000000 +00000-0 +13789-3 0 00008
2 05918 81.2339 91.2767 0057359 280.0565 79.4135 14.06305616 09
| Epoch (UTC): | 10 April 2026 05:19:53 |
| Eccentricity: | 0.0057359 |
| inclination: | 81.2339° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 91.2767° |
| argument of perigee: | 280.0565° |
| revolutions per day: | 14.06305616 |
| mean anomaly at epoch: | 79.4135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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