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 39444U 13066AE 24262.76683703 .00012048 00000-0 10982-2 0 9993
2 39444 97.7284 220.1699 0045799 185.8412 174.2280 14.94462480584660
| Epoch (UTC): | 18 September 2024 18:24:14 |
| Eccentricity: | 0.0045799 |
| inclination: | 97.7284° |
| perigee height: | 552 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 220.1699° |
| argument of perigee: | 185.8412° |
| revolutions per day: | 14.94462480 |
| mean anomaly at epoch: | 174.2280° |
| orbit number at epoch: | 58466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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