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 00649U 61015HA 24357.79305227 .00000174 00000-0 67042-3 0 9992
2 00649 66.2652 180.4437 0565105 301.8564 153.2994 12.65082950924145
| Epoch (UTC): | 22 December 2024 19:01:59 |
| Eccentricity: | 0.0565105 |
| inclination: | 66.2652° |
| perigee height: | 962 km |
| apogee height: | 1841 km |
| right ascension of ascending node: | 180.4437° |
| argument of perigee: | 301.8564° |
| revolutions per day: | 12.65082950 |
| mean anomaly at epoch: | 153.2994° |
| orbit number at epoch: | 92414 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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