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 22182.77601157 .00000093 00000-0 61200-4 0 9996
2 27844 98.6776 190.2455 0011024 64.0917 296.1396 14.22460593985904
| Epoch (UTC): | 01 July 2022 18:37:27 |
| Eccentricity: | 0.0011024 |
| inclination: | 98.6776° |
| perigee height: | 809 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 190.2455° |
| argument of perigee: | 64.0917° |
| revolutions per day: | 14.22460593 |
| mean anomaly at epoch: | 296.1396° |
| orbit number at epoch: | 98590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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