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 59904U 26145.42433529 +.00000000 +00000-0 +58052-4 0 00004
2 59904 43.0000 51.9345 0000917 255.7510 104.3240 15.27567501 08
| Epoch (UTC): | 25 May 2026 10:11:02 |
| Eccentricity: | 0.0000917 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 51.9345° |
| argument of perigee: | 255.7510° |
| revolutions per day: | 15.27567501 |
| mean anomaly at epoch: | 104.3240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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