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 28378U 26145.59372536 +.00000000 +00000-0 +00000-0 0 00009
2 28378 3.2307 79.7407 0004471 351.8556 274.1881 1.00271908 07
| Epoch (UTC): | 25 May 2026 14:14:57 |
| Eccentricity: | 0.0004471 |
| inclination: | 3.2307° |
| perigee height: | 35768 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 79.7407° |
| argument of perigee: | 351.8556° |
| revolutions per day: | 1.00271908 |
| mean anomaly at epoch: | 274.1881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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