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 60535U 24149BV 24358.14660979 .00008194 00000-0 77840-3 0 9994
2 60535 97.7387 71.5471 0002004 103.7413 256.4030 14.93747259 61943
| Epoch (UTC): | 23 December 2024 03:31:07 |
| Eccentricity: | 0.0002004 |
| inclination: | 97.7387° |
| perigee height: | 585 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 71.5471° |
| argument of perigee: | 103.7413° |
| revolutions per day: | 14.93747259 |
| mean anomaly at epoch: | 256.4030° |
| orbit number at epoch: | 6194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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