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 37746U 26063.00461683 +.00000000 +00000-0 +00000-0 0 00005
2 37746 5.0282 77.4204 0006227 187.8219 209.2344 0.98860945 06
| Epoch (UTC): | 04 March 2026 00:06:38 |
| Eccentricity: | 0.0006227 |
| inclination: | 5.0282° |
| perigee height: | 36160 km |
| apogee height: | 36213 km |
| right ascension of ascending node: | 77.4204° |
| argument of perigee: | 187.8219° |
| revolutions per day: | 0.98860945 |
| mean anomaly at epoch: | 209.2344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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