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 41634U 26072.01157616 +.00000000 +00000-0 +11418-3 0 00003
2 41634 75.0013 100.9949 0008674 268.5073 91.5122 14.93239309 07
| Epoch (UTC): | 13 March 2026 00:16:40 |
| Eccentricity: | 0.0008674 |
| inclination: | 75.0013° |
| perigee height: | 582 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 100.9949° |
| argument of perigee: | 268.5073° |
| revolutions per day: | 14.93239309 |
| mean anomaly at epoch: | 91.5122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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