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 25114U 97084C 24337.03070295 .00004571 00000-0 13632-2 0 9990
2 25114 45.0130 235.7806 0005525 308.0435 51.9916 14.44078968412996
| Epoch (UTC): | 02 December 2024 00:44:12 |
| Eccentricity: | 0.0005525 |
| inclination: | 45.0130° |
| perigee height: | 741 km |
| apogee height: | 749 km |
| right ascension of ascending node: | 235.7806° |
| argument of perigee: | 308.0435° |
| revolutions per day: | 14.44078968 |
| mean anomaly at epoch: | 51.9916° |
| orbit number at epoch: | 41299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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