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 43809U 26145.56996764 +.00000000 +00000-0 +27881-3 0 00006
2 43809 97.4237 197.7773 0015352 52.0736 308.1882 15.16092711 01
| Epoch (UTC): | 25 May 2026 13:40:45 |
| Eccentricity: | 0.0015352 |
| inclination: | 97.4237° |
| perigee height: | 507 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 197.7773° |
| argument of perigee: | 52.0736° |
| revolutions per day: | 15.16092711 |
| mean anomaly at epoch: | 308.1882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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