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 4157U 69082Z 23334.12530773 .00013989 00000-0 18058-2 0 9999
2 4157 70.0181 317.0419 0031146 41.6859 318.6656 14.80744300855294
| Epoch (UTC): | 30 November 2023 03:00:26 |
| Eccentricity: | 0.0031146 |
| inclination: | 70.0181° |
| perigee height: | 605 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 317.0419° |
| argument of perigee: | 41.6859° |
| revolutions per day: | 14.80744300 |
| mean anomaly at epoch: | 318.6656° |
| orbit number at epoch: | 85529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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