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 25012.70992629 .00014840 00000-0 86170-3 0 9997
2 40024 98.0828 1.1064 0005449 160.1299 200.0143 15.12223094574813
| Epoch (UTC): | 12 January 2025 17:02:17 |
| Eccentricity: | 0.0005449 |
| inclination: | 98.0828° |
| perigee height: | 525 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 1.1064° |
| argument of perigee: | 160.1299° |
| revolutions per day: | 15.12223094 |
| mean anomaly at epoch: | 200.0143° |
| orbit number at epoch: | 57481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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