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 41189U 26145.08468829 +.00000000 +00000-0 +15803-3 0 00009
2 41189 47.0037 19.8522 0001955 314.3061 45.7665 14.58841637 01
| Epoch (UTC): | 25 May 2026 02:01:57 |
| Eccentricity: | 0.0001955 |
| inclination: | 47.0037° |
| perigee height: | 696 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 19.8522° |
| argument of perigee: | 314.3061° |
| revolutions per day: | 14.58841637 |
| mean anomaly at epoch: | 45.7665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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