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 58220U 26145.44727756 +.00000000 +00000-0 -20045-2 0 00004
2 58220 43.0003 136.4644 0004695 100.2467 259.8907 15.06929959 06
| Epoch (UTC): | 25 May 2026 10:44:04 |
| Eccentricity: | 0.0004695 |
| inclination: | 43.0003° |
| perigee height: | 542 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 136.4644° |
| argument of perigee: | 100.2467° |
| revolutions per day: | 15.06929959 |
| mean anomaly at epoch: | 259.8907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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