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 59180U 26145.63103725 +.00000000 +00000-0 -71489-5 0 00006
2 59180 43.0009 18.4495 0001419 50.3348 309.7628 15.27606546 07
| Epoch (UTC): | 25 May 2026 15:08:41 |
| Eccentricity: | 0.0001419 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 18.4495° |
| argument of perigee: | 50.3348° |
| revolutions per day: | 15.27606546 |
| mean anomaly at epoch: | 309.7628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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