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 is defined by the following mean orbital elements,
1 39061U 13002A 25229.02356173 0.00000000 00000-0 00000-0 0 05
2 39061 97.4785 349.0630 0002541 264.4504 95.5495 15.17619384 05
| Epoch (UTC): | 17 August 2025 00:33:55 |
| Eccentricity: | 0.0002541 |
| inclination: | 97.4785° |
| perigee height: | 511 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 349.0630° |
| argument of perigee: | 264.4504° |
| revolutions per day: | 15.17619384 |
| mean anomaly at epoch: | 95.5495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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