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 60519U 24149BD 24357.79216958 .00016881 00000-0 70649-3 0 9992
2 60519 97.4271 71.6922 0007801 66.1205 294.0848 15.23609886 19458
| Epoch (UTC): | 22 December 2024 19:00:43 |
| Eccentricity: | 0.0007801 |
| inclination: | 97.4271° |
| perigee height: | 489 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 71.6922° |
| argument of perigee: | 66.1205° |
| revolutions per day: | 15.23609886 |
| mean anomaly at epoch: | 294.0848° |
| orbit number at epoch: | 1945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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