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 27939U 03042A 23340.77282368 .00001509 00000-0 26548-3 0 9997
2 27939 98.2649 129.3627 0011464 315.3536 151.5473 14.69062673 79873
| Epoch (UTC): | 06 December 2023 18:32:51 |
| Eccentricity: | 0.0011464 |
| inclination: | 98.2649° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 129.3627° |
| argument of perigee: | 315.3536° |
| revolutions per day: | 14.69062673 |
| mean anomaly at epoch: | 151.5473° |
| orbit number at epoch: | 7987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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