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 39056U 81053MU 25208.09842518 .00000839 00000-0 96227-3 0 9993
2 39056 82.9480 140.5698 0120821 261.8415 96.9017 13.65614297 35262
| Epoch (UTC): | 27 July 2025 02:21:43 |
| Eccentricity: | 0.0120821 |
| inclination: | 82.9480° |
| perigee height: | 926 km |
| apogee height: | 1104 km |
| right ascension of ascending node: | 140.5698° |
| argument of perigee: | 261.8415° |
| revolutions per day: | 13.65614297 |
| mean anomaly at epoch: | 96.9017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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