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 34056U 93036JT 23027.75591990 .00002110 00000-0 10919-2 0 9994
2 34056 74.0647 136.7225 0146184 79.4528 41.9632 14.10136369715599
| Epoch (UTC): | 27 January 2023 18:08:31 |
| Eccentricity: | 0.0146184 |
| inclination: | 74.0647° |
| perigee height: | 753 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 136.7225° |
| argument of perigee: | 79.4528° |
| revolutions per day: | 14.10136369 |
| mean anomaly at epoch: | 41.9632° |
| orbit number at epoch: | 71559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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