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 54422U 22151EW 24357.99757103 .00000495 00000-0 26654-3 0 9994
2 54422 98.8255 6.7138 0037955 102.3049 258.2378 14.16953643108960
| Epoch (UTC): | 22 December 2024 23:56:30 |
| Eccentricity: | 0.0037955 |
| inclination: | 98.8255° |
| perigee height: | 808 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 6.7138° |
| argument of perigee: | 102.3049° |
| revolutions per day: | 14.16953643 |
| mean anomaly at epoch: | 258.2378° |
| orbit number at epoch: | 10896 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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