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 24278U 96046B 22179.67175372 -.00000016 00000-0 22341-4 0 9991
2 24278 98.5151 201.8192 0349234 254.1595 102.0792 13.53116615277125
| Epoch (UTC): | 28 June 2022 16:07:19 |
| Eccentricity: | 0.0349234 |
| inclination: | 98.5151° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 201.8192° |
| argument of perigee: | 254.1595° |
| revolutions per day: | 13.53116615 |
| mean anomaly at epoch: | 102.0792° |
| orbit number at epoch: | 27712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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