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 56725U 23068R 24277.08210423 .00008214 00000-0 92823-3 0 9998
2 56725 86.6703 290.9145 0007676 235.7962 124.2536 14.86371968 75229
| Epoch (UTC): | 03 October 2024 01:58:13 |
| Eccentricity: | 0.0007676 |
| inclination: | 86.6703° |
| perigee height: | 604 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 290.9145° |
| argument of perigee: | 235.7962° |
| revolutions per day: | 14.86371968 |
| mean anomaly at epoch: | 124.2536° |
| orbit number at epoch: | 7522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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