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 00059U 60013B 23028.88793580 .00000159 00000-0 97595-4 0 9991
2 00059 28.2504 350.2483 0189114 25.6317 335.3468 13.53016478 75732
| Epoch (UTC): | 28 January 2023 21:18:37 |
| Eccentricity: | 0.0189114 |
| inclination: | 28.2504° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 350.2483° |
| argument of perigee: | 25.6317° |
| revolutions per day: | 13.53016478 |
| mean anomaly at epoch: | 335.3468° |
| orbit number at epoch: | 7573 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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