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 22175.60127980 .00000186 00000-0 10277-3 0 9997
2 27844 98.6777 183.1796 0011156 82.5450 277.6995 14.22457885984882
| Epoch (UTC): | 24 June 2022 14:25:50 |
| Eccentricity: | 0.0011156 |
| inclination: | 98.6777° |
| perigee height: | 809 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 183.1796° |
| argument of perigee: | 82.5450° |
| revolutions per day: | 14.22457885 |
| mean anomaly at epoch: | 277.6995° |
| orbit number at epoch: | 98488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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