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 58966U 26145.14652207 +.00000000 +00000-0 +81415-5 0 00006
2 58966 53.1614 301.2349 0001155 104.3692 255.7437 15.30193550 00
| Epoch (UTC): | 25 May 2026 03:30:59 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 301.2349° |
| argument of perigee: | 104.3692° |
| revolutions per day: | 15.30193550 |
| mean anomaly at epoch: | 255.7437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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