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 40912U 15049P 22268.53914119 .00010854 00000-0 40008-3 0 9991
2 40912 97.4373 279.5810 0010678 316.1556 164.5004 15.27935268389022
| Epoch (UTC): | 25 September 2022 12:56:21 |
| Eccentricity: | 0.0010678 |
| inclination: | 97.4373° |
| perigee height: | 474 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 279.5810° |
| argument of perigee: | 316.1556° |
| revolutions per day: | 15.27935268 |
| mean anomaly at epoch: | 164.5004° |
| orbit number at epoch: | 38902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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