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 60085U 24114G 24358.03432810 .00012705 00000-0 87439-3 0 9993
2 60085 98.0053 19.6446 0080949 132.8480 227.9583 15.03352428 27774
| Epoch (UTC): | 23 December 2024 00:49:25 |
| Eccentricity: | 0.0080949 |
| inclination: | 98.0053° |
| perigee height: | 500 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 19.6446° |
| argument of perigee: | 132.8480° |
| revolutions per day: | 15.03352428 |
| mean anomaly at epoch: | 227.9583° |
| orbit number at epoch: | 2777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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