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 40014U 14033E 23079.25197538 .00006617 00000-0 55183-3 0 9996
2 40014 98.1457 94.2547 0029643 199.3756 160.6331 14.98615307477417
| Epoch (UTC): | 20 March 2023 06:02:50 |
| Eccentricity: | 0.0029643 |
| inclination: | 98.1457° |
| perigee height: | 550 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 94.2547° |
| argument of perigee: | 199.3756° |
| revolutions per day: | 14.98615307 |
| mean anomaly at epoch: | 160.6331° |
| orbit number at epoch: | 47741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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