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 38978U 26145.47741927 +.00000000 +00000-0 +00000-0 0 00007
2 38978 0.0144 273.0697 0000756 307.8454 16.9581 1.00269874 06
| Epoch (UTC): | 25 May 2026 11:27:29 |
| Eccentricity: | 0.0000756 |
| inclination: | 0.0144° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 273.0697° |
| argument of perigee: | 307.8454° |
| revolutions per day: | 1.00269874 |
| mean anomaly at epoch: | 16.9581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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