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 39865U 92093LT 23150.17249601 .00001310 00000-0 49948-3 0 9997
2 39865 71.0154 317.7751 0006511 279.3313 80.7083 14.32683522 54824
| Epoch (UTC): | 30 May 2023 04:08:23 |
| Eccentricity: | 0.0006511 |
| inclination: | 71.0154° |
| perigee height: | 778 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 317.7751° |
| argument of perigee: | 279.3313° |
| revolutions per day: | 14.32683522 |
| mean anomaly at epoch: | 80.7083° |
| orbit number at epoch: | 5482 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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