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 28492U 04049A 24358.17314907 .00005453 00000-0 44721-3 0 9994
2 28492 98.3263 4.3007 0008624 312.0056 48.0431 14.99680146 72602
| Epoch (UTC): | 23 December 2024 04:09:20 |
| Eccentricity: | 0.0008624 |
| inclination: | 98.3263° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 4.3007° |
| argument of perigee: | 312.0056° |
| revolutions per day: | 14.99680146 |
| mean anomaly at epoch: | 48.0431° |
| orbit number at epoch: | 7260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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