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 60088U 24116A 24279.86792530 .00009385 00000-0 11745-2 0 9995
2 60088 28.9956 63.6694 0003900 217.8118 142.2201 14.80853483 15627
| Epoch (UTC): | 05 October 2024 20:49:48 |
| Eccentricity: | 0.0003900 |
| inclination: | 28.9956° |
| perigee height: | 624 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 63.6694° |
| argument of perigee: | 217.8118° |
| revolutions per day: | 14.80853483 |
| mean anomaly at epoch: | 142.2201° |
| orbit number at epoch: | 1562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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