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 25544U 98067A 23267.18358897 .00017598 00000-0 32006-3 0 9993
2 25544 51.6414 198.1738 0005906 52.6735 89.7966 15.49591051417140
| Epoch (UTC): | 24 September 2023 04:24:22 |
| Eccentricity: | 0.0005906 |
| inclination: | 51.6414° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 198.1738° |
| argument of perigee: | 52.6735° |
| revolutions per day: | 15.49591051 |
| mean anomaly at epoch: | 89.7966° |
| orbit number at epoch: | 41714 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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