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 03597U 68110A 23088.83828605 .00000601 00000-0 17117-3 0 9998
2 03597 34.9926 146.3917 0006031 222.0298 137.9930 14.46141901863241
| Epoch (UTC): | 29 March 2023 20:07:07 |
| Eccentricity: | 0.0006031 |
| inclination: | 34.9926° |
| perigee height: | 734 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 146.3917° |
| argument of perigee: | 222.0298° |
| revolutions per day: | 14.46141901 |
| mean anomaly at epoch: | 137.9930° |
| orbit number at epoch: | 86324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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