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 45443U 26145.36094280 +.00000000 +00000-0 +65922-3 0 00000
2 45443 87.8914 25.6072 0001693 80.7736 279.3583 13.11412453 03
| Epoch (UTC): | 25 May 2026 08:39:45 |
| Eccentricity: | 0.0001693 |
| inclination: | 87.8914° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6072° |
| argument of perigee: | 80.7736° |
| revolutions per day: | 13.11412453 |
| mean anomaly at epoch: | 279.3583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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