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 22176.93584906 -.00000002 00000-0 37107-4 0 9995
2 24278 98.5152 199.4593 0349217 261.2808 94.8637 13.53116457276758
| Epoch (UTC): | 25 June 2022 22:27:37 |
| Eccentricity: | 0.0349217 |
| inclination: | 98.5152° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 199.4593° |
| argument of perigee: | 261.2808° |
| revolutions per day: | 13.53116457 |
| mean anomaly at epoch: | 94.8637° |
| orbit number at epoch: | 27675 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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