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 23086.88221587 .00000745 00000-0 35194-3 0 9993
2 27844 98.6811 95.3244 0009919 8.5981 351.5365 14.22698453 24172
| Epoch (UTC): | 27 March 2023 21:10:23 |
| Eccentricity: | 0.0009919 |
| inclination: | 98.6811° |
| perigee height: | 809 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 95.3244° |
| argument of perigee: | 8.5981° |
| revolutions per day: | 14.22698453 |
| mean anomaly at epoch: | 351.5365° |
| orbit number at epoch: | 2417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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