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 52157U 22033A 23336.76084069 .00005706 00000-0 75831-3 0 9992
2 52157 97.9082 57.1384 0015078 73.7332 286.5537 14.80060124 90226
| Epoch (UTC): | 02 December 2023 18:15:36 |
| Eccentricity: | 0.0015078 |
| inclination: | 97.9082° |
| perigee height: | 618 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 57.1384° |
| argument of perigee: | 73.7332° |
| revolutions per day: | 14.80060124 |
| mean anomaly at epoch: | 286.5537° |
| orbit number at epoch: | 9022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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