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 39362U 13058C 25196.04630102 .00002335 00000-0 59643-3 0 9992
2 39362 49.5524 201.9600 5131422 326.3092 9.6808 5.37288495225365
| Epoch (UTC): | 15 July 2025 01:06:40 |
| Eccentricity: | 0.5131422 |
| inclination: | 49.5524° |
| perigee height: | 326 km |
| apogee height: | 14457 km |
| right ascension of ascending node: | 201.9600° |
| argument of perigee: | 326.3092° |
| revolutions per day: | 5.37288495 |
| mean anomaly at epoch: | 9.6808° |
| orbit number at epoch: | 22536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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