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 24357.41547657 .00000125 00000-0 52108-4 0 9992
2 00059 28.2496 27.2732 0189095 87.3278 274.8895 13.53114982169733
| Epoch (UTC): | 22 December 2024 09:58:17 |
| Eccentricity: | 0.0189095 |
| inclination: | 28.2496° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 27.2732° |
| argument of perigee: | 87.3278° |
| revolutions per day: | 13.53114982 |
| mean anomaly at epoch: | 274.8895° |
| orbit number at epoch: | 16973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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