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 25414U 98046B 24358.11395831 .00003119 00000-0 10769-2 0 9995
2 25414 44.9931 290.1297 0003599 94.8310 265.2949 14.37585997379070
| Epoch (UTC): | 23 December 2024 02:44:05 |
| Eccentricity: | 0.0003599 |
| inclination: | 44.9931° |
| perigee height: | 764 km |
| apogee height: | 769 km |
| right ascension of ascending node: | 290.1297° |
| argument of perigee: | 94.8310° |
| revolutions per day: | 14.37585997 |
| mean anomaly at epoch: | 265.2949° |
| orbit number at epoch: | 37907 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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