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 39425U 13066K 24260.94799959 .00003781 00000-0 44351-3 0 9993
2 39425 97.7372 210.6844 0047233 223.0074 136.7445 14.84751465585128
| Epoch (UTC): | 16 September 2024 22:45:07 |
| Eccentricity: | 0.0047233 |
| inclination: | 97.7372° |
| perigee height: | 581 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 210.6844° |
| argument of perigee: | 223.0074° |
| revolutions per day: | 14.84751465 |
| mean anomaly at epoch: | 136.7445° |
| orbit number at epoch: | 58512 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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