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 24256.93053331 .00000239 00000-0 20104-3 0 9994
2 00059 28.2481 183.5542 0188846 323.7350 35.0525 13.53089138156112
| Epoch (UTC): | 12 September 2024 22:19:58 |
| Eccentricity: | 0.0188846 |
| inclination: | 28.2481° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 183.5542° |
| argument of perigee: | 323.7350° |
| revolutions per day: | 13.53089138 |
| mean anomaly at epoch: | 35.0525° |
| orbit number at epoch: | 15611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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