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 27909U 84069AB 22172.09572340 .00000092 00000-0 14293-3 0 9991
2 27909 65.0494 59.2371 0037741 168.4336 191.7604 13.91533277449294
| Epoch (UTC): | 21 June 2022 02:17:50 |
| Eccentricity: | 0.0037741 |
| inclination: | 65.0494° |
| perigee height: | 896 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 59.2371° |
| argument of perigee: | 168.4336° |
| revolutions per day: | 13.91533277 |
| mean anomaly at epoch: | 191.7604° |
| orbit number at epoch: | 44929 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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