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 30010U 99025MK 24357.46534671 .00000646 00000-0 28982-3 0 9994
2 30010 99.0674 171.7312 0073970 149.9076 238.5531 14.24643068932015
| Epoch (UTC): | 22 December 2024 11:10:05 |
| Eccentricity: | 0.0073970 |
| inclination: | 99.0674° |
| perigee height: | 756 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 171.7312° |
| argument of perigee: | 149.9076° |
| revolutions per day: | 14.24643068 |
| mean anomaly at epoch: | 238.5531° |
| orbit number at epoch: | 93201 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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