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 59443U 26145.38684102 +.00000000 +00000-0 +36322-3 0 00007
2 59443 45.5953 34.5081 0003904 290.1503 69.8958 14.99024040 03
| Epoch (UTC): | 25 May 2026 09:17:03 |
| Eccentricity: | 0.0003904 |
| inclination: | 45.5953° |
| perigee height: | 567 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 34.5081° |
| argument of perigee: | 290.1503° |
| revolutions per day: | 14.99024040 |
| mean anomaly at epoch: | 69.8958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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