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 34572U 93036VJ 24358.16522934 .00017825 00000-0 52335-2 0 9999
2 34572 74.0146 58.4001 0074563 222.1106 167.7862 14.42151513822503
| Epoch (UTC): | 23 December 2024 03:57:55 |
| Eccentricity: | 0.0074563 |
| inclination: | 74.0146° |
| perigee height: | 698 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 58.4001° |
| argument of perigee: | 222.1106° |
| revolutions per day: | 14.42151513 |
| mean anomaly at epoch: | 167.7862° |
| orbit number at epoch: | 82250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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