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 26474U 00047B 24357.87294583 .00006311 00000-0 44240-3 0 9999
2 26474 67.9905 198.8319 0045668 183.1429 176.9439 15.04985136326324
| Epoch (UTC): | 22 December 2024 20:57:02 |
| Eccentricity: | 0.0045668 |
| inclination: | 67.9905° |
| perigee height: | 520 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 198.8319° |
| argument of perigee: | 183.1429° |
| revolutions per day: | 15.04985136 |
| mean anomaly at epoch: | 176.9439° |
| orbit number at epoch: | 32632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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