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 41937U 26146.22955610 +.00000000 +00000-0 +00000-0 0 00006
2 41937 2.2031 42.7010 0002320 14.7079 289.9313 1.00272284 04
| Epoch (UTC): | 26 May 2026 05:30:33 |
| Eccentricity: | 0.0002320 |
| inclination: | 2.2031° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 42.7010° |
| argument of perigee: | 14.7079° |
| revolutions per day: | 1.00272284 |
| mean anomaly at epoch: | 289.9313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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