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 24251.78226801 .00000210 00000-0 25084-3 0 9991
2 24278 98.5792 175.6055 0349698 334.5058 23.9185 13.53207188385609
| Epoch (UTC): | 07 September 2024 18:46:27 |
| Eccentricity: | 0.0349698 |
| inclination: | 98.5792° |
| perigee height: | 800 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 175.6055° |
| argument of perigee: | 334.5058° |
| revolutions per day: | 13.53207188 |
| mean anomaly at epoch: | 23.9185° |
| orbit number at epoch: | 38560 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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