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 13778U 83004B 24276.82566106 .00000712 00000-0 43771-3 0 9991
2 13778 100.0706 244.2741 0021040 164.6526 195.5282 14.09445098142040
| Epoch (UTC): | 02 October 2024 19:48:57 |
| Eccentricity: | 0.0021040 |
| inclination: | 100.0706° |
| perigee height: | 846 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 244.2741° |
| argument of perigee: | 164.6526° |
| revolutions per day: | 14.09445098 |
| mean anomaly at epoch: | 195.5282° |
| orbit number at epoch: | 14204 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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