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 54993U 22151UJ 24358.22628607 .00001928 00000-0 11080-2 0 9998
2 54993 98.8333 356.6066 0052360 70.0927 290.5874 14.09756334107510
| Epoch (UTC): | 23 December 2024 05:25:51 |
| Eccentricity: | 0.0052360 |
| inclination: | 98.8333° |
| perigee height: | 822 km |
| apogee height: | 898 km |
| right ascension of ascending node: | 356.6066° |
| argument of perigee: | 70.0927° |
| revolutions per day: | 14.09756334 |
| mean anomaly at epoch: | 290.5874° |
| orbit number at epoch: | 10751 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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