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 is defined by the following mean orbital elements,
1 40869U 12008AK 25084.12490536 .00001642 00000-0 64908-1 0 9998
2 40869 18.4629 332.1874 7262155 75.3839 348.9966 2.08076564 89910
| Epoch (UTC): | 25 March 2025 02:59:51 |
| Eccentricity: | 0.7262155 |
| inclination: | 18.4629° |
| perigee height: | 717 km |
| apogee height: | 38360 km |
| right ascension of ascending node: | 332.1874° |
| argument of perigee: | 75.3839° |
| revolutions per day: | 2.08076564 |
| mean anomaly at epoch: | 348.9966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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