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 30231U 99025WQ 24357.62890059 .00002348 00000-0 12423-2 0 9995
2 30231 98.8481 42.3528 0129503 313.9766 198.1420 14.10510485920115
| Epoch (UTC): | 22 December 2024 15:05:37 |
| Eccentricity: | 0.0129503 |
| inclination: | 98.8481° |
| perigee height: | 764 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 42.3528° |
| argument of perigee: | 313.9766° |
| revolutions per day: | 14.10510485 |
| mean anomaly at epoch: | 198.1420° |
| orbit number at epoch: | 92011 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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