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 41183U 26088.21250854 +.00000000 +00000-0 +26206-3 0 00000
2 41183 47.0058 19.8728 0003091 11.3491 348.7464 14.58767442 04
| Epoch (UTC): | 29 March 2026 05:06:00 |
| Eccentricity: | 0.0003091 |
| inclination: | 47.0058° |
| perigee height: | 695 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 19.8728° |
| argument of perigee: | 11.3491° |
| revolutions per day: | 14.58767442 |
| mean anomaly at epoch: | 348.7464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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