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 26087.82767840 +.00000000 +00000-0 +17508-3 0 00005
2 41189 47.0020 290.5495 0001308 45.4223 314.6769 14.58766209 08
| Epoch (UTC): | 28 March 2026 19:51:51 |
| Eccentricity: | 0.0001308 |
| inclination: | 47.0020° |
| perigee height: | 696 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 290.5495° |
| argument of perigee: | 45.4223° |
| revolutions per day: | 14.58766209 |
| mean anomaly at epoch: | 314.6769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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