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 27846U 03031G 23082.72883203 .00000572 00000-0 27528-3 0 9993
2 27846 98.6888 90.2697 0009162 355.3133 4.7958 14.22632228 23628
| Epoch (UTC): | 23 March 2023 17:29:31 |
| Eccentricity: | 0.0009162 |
| inclination: | 98.6888° |
| perigee height: | 810 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 90.2697° |
| argument of perigee: | 355.3133° |
| revolutions per day: | 14.22632228 |
| mean anomaly at epoch: | 4.7958° |
| orbit number at epoch: | 2362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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