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 04621U 70089H 24357.90142957 .00008397 00000-0 23565-2 0 9995
2 04621 62.9145 177.7547 0698997 153.8885 209.9236 13.56200032608003
| Epoch (UTC): | 22 December 2024 21:38:03 |
| Eccentricity: | 0.0698997 |
| inclination: | 62.9145° |
| perigee height: | 530 km |
| apogee height: | 1569 km |
| right ascension of ascending node: | 177.7547° |
| argument of perigee: | 153.8885° |
| revolutions per day: | 13.56200032 |
| mean anomaly at epoch: | 209.9236° |
| orbit number at epoch: | 60800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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