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 14780U 84021A 23277.61652569 .00004144 00000-0 35370-3 0 9990
2 14780 98.1510 140.1978 0084394 165.0980 195.2756 14.95546801643453
| Epoch (UTC): | 04 October 2023 14:47:47 |
| Eccentricity: | 0.0084394 |
| inclination: | 98.1510° |
| perigee height: | 522 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 140.1978° |
| argument of perigee: | 165.0980° |
| revolutions per day: | 14.95546801 |
| mean anomaly at epoch: | 195.2756° |
| orbit number at epoch: | 64345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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