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 37854U 11061E 23083.58410715 .00058289 00000-0 20285-2 0 9994
2 37854 101.6909 1.5363 0117366 279.2172 79.5790 15.23091780624495
| Epoch (UTC): | 24 March 2023 14:01:06 |
| Eccentricity: | 0.0117366 |
| inclination: | 101.6909° |
| perigee height: | 416 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 1.5363° |
| argument of perigee: | 279.2172° |
| revolutions per day: | 15.23091780 |
| mean anomaly at epoch: | 79.5790° |
| orbit number at epoch: | 62449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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