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 30218U 99025WB 24357.16184286 .00011493 00000-0 49306-2 0 9998
2 30218 98.9992 71.1311 0077446 201.4235 188.7328 14.23312090920408
| Epoch (UTC): | 22 December 2024 03:53:03 |
| Eccentricity: | 0.0077446 |
| inclination: | 98.9992° |
| perigee height: | 758 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 71.1311° |
| argument of perigee: | 201.4235° |
| revolutions per day: | 14.23312090 |
| mean anomaly at epoch: | 188.7328° |
| orbit number at epoch: | 92040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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