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 25080.57982194 .00011393 00000-0 70423-3 0 9996
2 40014 98.0833 142.7920 0030632 279.6608 80.1160 15.09643501587414
| Epoch (UTC): | 21 March 2025 13:54:56 |
| Eccentricity: | 0.0030632 |
| inclination: | 98.0833° |
| perigee height: | 516 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 142.7920° |
| argument of perigee: | 279.6608° |
| revolutions per day: | 15.09643501 |
| mean anomaly at epoch: | 80.1160° |
| orbit number at epoch: | 58741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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