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 38551U 26145.56258167 +.00000000 +00000-0 +00000-0 0 00003
2 38551 0.0179 311.2446 0002222 115.8746 271.4551 1.00270257 01
| Epoch (UTC): | 25 May 2026 13:30:07 |
| Eccentricity: | 0.0002222 |
| inclination: | 0.0179° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 311.2446° |
| argument of perigee: | 115.8746° |
| revolutions per day: | 1.00270257 |
| mean anomaly at epoch: | 271.4551° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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