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 41006U 26063.92160738 +.00000000 +00000-0 +22718-2 0 00009
2 41006 102.3691 325.7143 0183051 174.5622 185.7566 13.85952781 02
| Epoch (UTC): | 04 March 2026 22:07:06 |
| Eccentricity: | 0.0183051 |
| inclination: | 102.3691° |
| perigee height: | 809 km |
| apogee height: | 1077 km |
| right ascension of ascending node: | 325.7143° |
| argument of perigee: | 174.5622° |
| revolutions per day: | 13.85952781 |
| mean anomaly at epoch: | 185.7566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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