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 27598U 02056B 24337.15699660 .00000540 00000-0 22949-3 0 9993
2 27598 98.7812 292.5142 0009029 170.1052 190.0308 14.29412572145467
| Epoch (UTC): | 02 December 2024 03:46:04 |
| Eccentricity: | 0.0009029 |
| inclination: | 98.7812° |
| perigee height: | 787 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 292.5142° |
| argument of perigee: | 170.1052° |
| revolutions per day: | 14.29412572 |
| mean anomaly at epoch: | 190.0308° |
| orbit number at epoch: | 14546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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