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 39090U 13009E 24357.50901070 .00000781 00000-0 28034-3 0 9993
2 39090 98.3765 180.6797 0009663 54.2262 305.9822 14.36529834619273
| Epoch (UTC): | 22 December 2024 12:12:58 |
| Eccentricity: | 0.0009663 |
| inclination: | 98.3765° |
| perigee height: | 763 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 180.6797° |
| argument of perigee: | 54.2262° |
| revolutions per day: | 14.36529834 |
| mean anomaly at epoch: | 305.9822° |
| orbit number at epoch: | 61927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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