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 40024U 14033Q 25349.94119790 .00012061 00000-0 49003-3 0 9993
2 40024 98.0899 1.8525 0005837 97.0539 263.1360 15.24725761625994
| Epoch (UTC): | 15 December 2025 22:35:19 |
| Eccentricity: | 0.0005837 |
| inclination: | 98.0899° |
| perigee height: | 487 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 1.8525° |
| argument of perigee: | 97.0539° |
| revolutions per day: | 15.24725761 |
| mean anomaly at epoch: | 263.1360° |
| orbit number at epoch: | 62599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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