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 26075.81847786 +.00000000 +00000-0 -48057-4 0 00004
2 05918 81.2350 114.9111 0057696 350.1440 9.8591 14.06300505 08
| Epoch (UTC): | 16 March 2026 19:38:36 |
| Eccentricity: | 0.0057696 |
| inclination: | 81.2350° |
| perigee height: | 830 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 114.9111° |
| argument of perigee: | 350.1440° |
| revolutions per day: | 14.06300505 |
| mean anomaly at epoch: | 9.8591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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