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 22176.86190586 -.00000002 00000-0 37038-4 0 9997
2 24278 98.5152 199.3955 0349217 261.4732 94.6695 13.53116448276995
| Epoch (UTC): | 25 June 2022 20:41:08 |
| Eccentricity: | 0.0349217 |
| inclination: | 98.5152° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 199.3955° |
| argument of perigee: | 261.4732° |
| revolutions per day: | 13.53116448 |
| mean anomaly at epoch: | 94.6695° |
| orbit number at epoch: | 27699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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