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 20898U 90081BJ 24358.10311642 .00044846 00000-0 44180-2 0 9990
2 20898 98.1685 45.8741 0021765 207.4284 182.6225 14.91695118801238
| Epoch (UTC): | 23 December 2024 02:28:29 |
| Eccentricity: | 0.0021765 |
| inclination: | 98.1685° |
| perigee height: | 577 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 45.8741° |
| argument of perigee: | 207.4284° |
| revolutions per day: | 14.91695118 |
| mean anomaly at epoch: | 182.6225° |
| orbit number at epoch: | 80123 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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