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 23029.84715258 .00000154 00000-0 92059-4 0 9999
2 00059 28.2503 345.3208 0189126 33.6831 327.5578 13.53016595 75863
| Epoch (UTC): | 29 January 2023 20:19:53 |
| Eccentricity: | 0.0189126 |
| inclination: | 28.2503° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 345.3208° |
| argument of perigee: | 33.6831° |
| revolutions per day: | 13.53016595 |
| mean anomaly at epoch: | 327.5578° |
| orbit number at epoch: | 7586 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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