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 43759U 26145.38656646 +.00000000 +00000-0 +23644-3 0 00005
2 43759 97.4269 194.9879 0009316 29.9336 330.2427 15.14305745 01
| Epoch (UTC): | 25 May 2026 09:16:39 |
| Eccentricity: | 0.0009316 |
| inclination: | 97.4269° |
| perigee height: | 517 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 194.9879° |
| argument of perigee: | 29.9336° |
| revolutions per day: | 15.14305745 |
| mean anomaly at epoch: | 330.2427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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