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 23333.99396862 .00000788 00000-0 36943-3 0 9999
2 27844 98.6789 338.8558 0009937 11.7886 348.3523 14.22980546 59343
| Epoch (UTC): | 29 November 2023 23:51:18 |
| Eccentricity: | 0.0009937 |
| inclination: | 98.6789° |
| perigee height: | 808 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 338.8558° |
| argument of perigee: | 11.7886° |
| revolutions per day: | 14.22980546 |
| mean anomaly at epoch: | 348.3523° |
| orbit number at epoch: | 5934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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