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 43808U 26145.61786124 +.00000000 +00000-0 +57038-3 0 00005
2 43808 97.4690 218.0367 0005667 63.0143 297.1680 15.36940317 00
| Epoch (UTC): | 25 May 2026 14:49:43 |
| Eccentricity: | 0.0005667 |
| inclination: | 97.4690° |
| perigee height: | 451 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 218.0367° |
| argument of perigee: | 63.0143° |
| revolutions per day: | 15.36940317 |
| mean anomaly at epoch: | 297.1680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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