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 23342.13663115 .00001215 00000-0 21555-3 0 9999
2 27939 98.2650 130.7421 0011398 310.7290 164.5496 14.69066234 80075
| Epoch (UTC): | 08 December 2023 03:16:44 |
| Eccentricity: | 0.0011398 |
| inclination: | 98.2650° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 130.7421° |
| argument of perigee: | 310.7290° |
| revolutions per day: | 14.69066234 |
| mean anomaly at epoch: | 164.5496° |
| orbit number at epoch: | 8007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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