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 data is extracted from the following two-line orbital elements,
1 39440U 13066AA 23085.84085453 .00005254 00000-0 68890-3 0 9991
2 39440 97.7646 37.3588 0074601 295.7946 63.5582 14.78794160501984
| Epoch (UTC): | 26 March 2023 20:10:49 |
| Eccentricity: | 0.0074601 |
| inclination: | 97.7646° |
| perigee height: | 581 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 37.3588° |
| argument of perigee: | 295.7946° |
| revolutions per day: | 14.78794160 |
| mean anomaly at epoch: | 63.5582° |
| orbit number at epoch: | 50198 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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