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 23332.58767352 .00000811 00000-0 37928-3 0 9990
2 27844 98.6790 337.4699 0010043 15.7873 344.3616 14.22977993 59145
| Epoch (UTC): | 28 November 2023 14:06:14 |
| Eccentricity: | 0.0010043 |
| inclination: | 98.6790° |
| perigee height: | 808 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 337.4699° |
| argument of perigee: | 15.7873° |
| revolutions per day: | 14.22977993 |
| mean anomaly at epoch: | 344.3616° |
| orbit number at epoch: | 5914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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