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 24357.91206181 .00009130 00000-0 59026-3 0 9997
2 40014 98.1002 49.3415 0032195 217.7243 142.1726 15.08026724574041
| Epoch (UTC): | 22 December 2024 21:53:22 |
| Eccentricity: | 0.0032195 |
| inclination: | 98.1002° |
| perigee height: | 520 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 49.3415° |
| argument of perigee: | 217.7243° |
| revolutions per day: | 15.08026724 |
| mean anomaly at epoch: | 142.1726° |
| orbit number at epoch: | 57404 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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