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 60235U 24128A 24255.92980639 .00007148 00000-0 65488-3 0 9991
2 60235 61.9969 300.7411 0019457 309.3887 50.5476 14.95600959 9585
| Epoch (UTC): | 11 September 2024 22:18:55 |
| Eccentricity: | 0.0019457 |
| inclination: | 61.9969° |
| perigee height: | 567 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 300.7411° |
| argument of perigee: | 309.3887° |
| revolutions per day: | 14.95600959 |
| mean anomaly at epoch: | 50.5476° |
| orbit number at epoch: | 958 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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