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 60013U 24110B 24358.20921778 .00015047 00000-0 87745-3 0 9997
2 60013 97.5923 82.8864 0011148 335.1472 24.9220 15.12014815 30159
| Epoch (UTC): | 23 December 2024 05:01:16 |
| Eccentricity: | 0.0011148 |
| inclination: | 97.5923° |
| perigee height: | 522 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 82.8864° |
| argument of perigee: | 335.1472° |
| revolutions per day: | 15.12014815 |
| mean anomaly at epoch: | 24.9220° |
| orbit number at epoch: | 3015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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