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 39202U 13035A 24358.16671943 .00001724 00000-0 34100-3 0 9992
2 39202 98.2605 169.1349 0011534 126.7683 233.4579 14.63606426610051
| Epoch (UTC): | 23 December 2024 04:00:04 |
| Eccentricity: | 0.0011534 |
| inclination: | 98.2605° |
| perigee height: | 673 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 169.1349° |
| argument of perigee: | 126.7683° |
| revolutions per day: | 14.63606426 |
| mean anomaly at epoch: | 233.4579° |
| orbit number at epoch: | 61005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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