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 54427U 22151FB 24357.93351368 .00001609 00000-0 13203-2 0 9999
2 54427 98.9955 336.2144 0176436 176.5282 183.7143 13.83836369106396
| Epoch (UTC): | 22 December 2024 22:24:15 |
| Eccentricity: | 0.0176436 |
| inclination: | 98.9955° |
| perigee height: | 821 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 336.2144° |
| argument of perigee: | 176.5282° |
| revolutions per day: | 13.83836369 |
| mean anomaly at epoch: | 183.7143° |
| orbit number at epoch: | 10639 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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