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 22137.24695770 .00001638 00000-0 14834-3 0 9996
2 40014 98.1438 134.3859 0031376 138.8811 221.4786 14.96545600431476
| Epoch (UTC): | 17 May 2022 05:55:37 |
| Eccentricity: | 0.0031376 |
| inclination: | 98.1438° |
| perigee height: | 556 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 134.3859° |
| argument of perigee: | 138.8811° |
| revolutions per day: | 14.96545600 |
| mean anomaly at epoch: | 221.4786° |
| orbit number at epoch: | 43147 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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