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 27844U 03031E 22180.59545746 .00000129 00000-0 77466-4 0 9996
2 27844 98.6776 188.0980 0011085 69.7161 290.5208 14.22459972985596
| Epoch (UTC): | 29 June 2022 14:17:27 |
| Eccentricity: | 0.0011085 |
| inclination: | 98.6776° |
| perigee height: | 809 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 188.0980° |
| argument of perigee: | 69.7161° |
| revolutions per day: | 14.22459972 |
| mean anomaly at epoch: | 290.5208° |
| orbit number at epoch: | 98559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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