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 59489U 26145.03985468 +.00000000 +00000-0 -18986-4 0 00006
2 59489 43.0051 268.4466 0001766 280.2523 79.8130 15.27572642 07
| Epoch (UTC): | 25 May 2026 00:57:23 |
| Eccentricity: | 0.0001766 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 268.4466° |
| argument of perigee: | 280.2523° |
| revolutions per day: | 15.27572642 |
| mean anomaly at epoch: | 79.8130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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