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 23079.77899378 .00000629 00000-0 30037-3 0 9994
2 27844 98.6810 88.3245 0010320 28.3676 331.8062 14.22686530 23169
| Epoch (UTC): | 20 March 2023 18:41:45 |
| Eccentricity: | 0.0010320 |
| inclination: | 98.6810° |
| perigee height: | 809 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 88.3245° |
| argument of perigee: | 28.3676° |
| revolutions per day: | 14.22686530 |
| mean anomaly at epoch: | 331.8062° |
| orbit number at epoch: | 2316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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