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 54109U 22137A 24357.95555455 .00016094 00000-0 45561-3 0 9992
2 54109 96.9960 69.2677 0012718 199.9171 160.1580 15.36280311122830
| Epoch (UTC): | 22 December 2024 22:55:59 |
| Eccentricity: | 0.0012718 |
| inclination: | 96.9960° |
| perigee height: | 448 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 69.2677° |
| argument of perigee: | 199.9171° |
| revolutions per day: | 15.36280311 |
| mean anomaly at epoch: | 160.1580° |
| orbit number at epoch: | 12283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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