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 38254U 26145.58043508 +.00000000 +00000-0 +00000-0 0 00006
2 38254 6.5992 57.6520 0002424 356.9478 21.0582 1.00271393 08
| Epoch (UTC): | 25 May 2026 13:55:49 |
| Eccentricity: | 0.0002424 |
| inclination: | 6.5992° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 57.6520° |
| argument of perigee: | 356.9478° |
| revolutions per day: | 1.00271393 |
| mean anomaly at epoch: | 21.0582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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