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 22180.55907679 -.00000024 00000-0 13830-4 0 9995
2 24278 98.5150 202.5845 0349235 251.8500 104.4324 13.53116653277240
| Epoch (UTC): | 29 June 2022 13:25:04 |
| Eccentricity: | 0.0349235 |
| inclination: | 98.5150° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 202.5845° |
| argument of perigee: | 251.8500° |
| revolutions per day: | 13.53116653 |
| mean anomaly at epoch: | 104.4324° |
| orbit number at epoch: | 27724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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