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 20442U 90005G 24340.56147771 .00000546 00000-0 21318-3 0 9990
2 20442 98.8943 335.4744 0012474 47.2547 312.9684 14.33783753822337
| Epoch (UTC): | 05 December 2024 13:28:31 |
| Eccentricity: | 0.0012474 |
| inclination: | 98.8943° |
| perigee height: | 770 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 335.4744° |
| argument of perigee: | 47.2547° |
| revolutions per day: | 14.33783753 |
| mean anomaly at epoch: | 312.9684° |
| orbit number at epoch: | 82233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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