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 13649U 82109B 25193.89537310 .00000200 00000-0 74012-4 0 9999
2 13649 74.0013 336.5261 0017885 164.1154 6.3448 14.38440256234884
| Epoch (UTC): | 12 July 2025 21:29:20 |
| Eccentricity: | 0.0017885 |
| inclination: | 74.0013° |
| perigee height: | 751 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 336.5261° |
| argument of perigee: | 164.1154° |
| revolutions per day: | 14.38440256 |
| mean anomaly at epoch: | 6.3448° |
| orbit number at epoch: | 23488 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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