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 64258U 26145.58335647 +.00000000 +00000-0 -46294-3 0 00006
2 64258 53.1586 117.2568 0001265 88.4124 175.8140 15.35380815 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1586° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 117.2568° |
| argument of perigee: | 88.4124° |
| revolutions per day: | 15.35380815 |
| mean anomaly at epoch: | 175.8140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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