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 23339.75975355 .00000584 00000-0 27852-3 0 9992
2 27844 98.6790 344.5378 0009621 355.1621 4.9463 14.22989721 60165
| Epoch (UTC): | 05 December 2023 18:14:02 |
| Eccentricity: | 0.0009621 |
| inclination: | 98.6790° |
| perigee height: | 808 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 344.5378° |
| argument of perigee: | 355.1621° |
| revolutions per day: | 14.22989721 |
| mean anomaly at epoch: | 4.9463° |
| orbit number at epoch: | 6016 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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