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 24357.89960243 .00003067 00000-0 50296-3 0 9992
2 27939 98.3082 157.5499 0011637 178.8573 338.5629 14.71421059135884
| Epoch (UTC): | 22 December 2024 21:35:25 |
| Eccentricity: | 0.0011637 |
| inclination: | 98.3082° |
| perigee height: | 648 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 157.5499° |
| argument of perigee: | 178.8573° |
| revolutions per day: | 14.71421059 |
| mean anomaly at epoch: | 338.5629° |
| orbit number at epoch: | 13588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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