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 38758U 12048A 26010.74405844 0.00000000 00000-0 00000-0 0 04
2 38758 63.4226 250.6733 0297789 358.2976 1.7024 13.40991135 04
| Epoch (UTC): | 10 January 2026 17:51:26 |
| Eccentricity: | 0.0297789 |
| inclination: | 63.4226° |
| perigee height: | 883 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 250.6733° |
| argument of perigee: | 358.2976° |
| revolutions per day: | 13.40991135 |
| mean anomaly at epoch: | 1.7024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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