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 08314U 72058EG 24357.53276259 .00008405 00000-0 86253-3 0 9992
2 08314 98.4806 185.6497 0078208 183.0508 177.0240 14.88418711767096
| Epoch (UTC): | 22 December 2024 12:47:10 |
| Eccentricity: | 0.0078208 |
| inclination: | 98.4806° |
| perigee height: | 548 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 185.6497° |
| argument of perigee: | 183.0508° |
| revolutions per day: | 14.88418711 |
| mean anomaly at epoch: | 177.0240° |
| orbit number at epoch: | 76709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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