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 23335.07873060 .00000187 00000-0 13486-3 0 9992
2 00059 28.2466 217.2701 0189036 75.7978 286.3489 13.53049726117238
| Epoch (UTC): | 01 December 2023 01:53:22 |
| Eccentricity: | 0.0189036 |
| inclination: | 28.2466° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 217.2701° |
| argument of perigee: | 75.7978° |
| revolutions per day: | 13.53049726 |
| mean anomaly at epoch: | 286.3489° |
| orbit number at epoch: | 11723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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