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 41105U 26088.18367372 +.00000000 +00000-0 +00000-0 0 00005
2 41105 6.4940 71.4927 0002847 246.0030 280.7222 1.00271812 07
| Epoch (UTC): | 29 March 2026 04:24:29 |
| Eccentricity: | 0.0002847 |
| inclination: | 6.4940° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 71.4927° |
| argument of perigee: | 246.0030° |
| revolutions per day: | 1.00271812 |
| mean anomaly at epoch: | 280.7222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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