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 58959U 26145.32842027 +.00000000 +00000-0 +39581-4 0 00005
2 58959 39.9887 147.9868 0010868 128.0629 232.1100 13.70554808 06
| Epoch (UTC): | 25 May 2026 07:52:55 |
| Eccentricity: | 0.0010868 |
| inclination: | 39.9887° |
| perigee height: | 990 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 147.9868° |
| argument of perigee: | 128.0629° |
| revolutions per day: | 13.70554808 |
| mean anomaly at epoch: | 232.1100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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