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 40967U 15058D 22173.39270692 .00001190 00000-0 13961-3 0 4009
2 40967 64.7759 57.0150 0194643 198.9014 160.4799 14.77428915 61396
| Epoch (UTC): | 22 June 2022 09:25:29 |
| Eccentricity: | 0.0194643 |
| inclination: | 64.7759° |
| perigee height: | 501 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 57.0150° |
| argument of perigee: | 198.9014° |
| revolutions per day: | 14.77428915 |
| mean anomaly at epoch: | 160.4799° |
| orbit number at epoch: | 6139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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