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 39323U 94029AFJ 24355.73199790 .00009550 00000-0 13891-2 0 9991
2 39323 81.9897 162.7849 0187902 271.2573 86.7111 14.64434731136309
| Epoch (UTC): | 20 December 2024 17:34:04 |
| Eccentricity: | 0.0187902 |
| inclination: | 81.9897° |
| perigee height: | 546 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 162.7849° |
| argument of perigee: | 271.2573° |
| revolutions per day: | 14.64434731 |
| mean anomaly at epoch: | 86.7111° |
| orbit number at epoch: | 13630 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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