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 55918U 26145.32322992 +.00000000 +00000-0 +24903-4 0 00003
2 55918 69.9992 111.3385 0003926 264.1506 95.9205 14.98332732 02
| Epoch (UTC): | 25 May 2026 07:45:27 |
| Eccentricity: | 0.0003926 |
| inclination: | 69.9992° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 111.3385° |
| argument of perigee: | 264.1506° |
| revolutions per day: | 14.98332732 |
| mean anomaly at epoch: | 95.9205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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