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 39078U 26145.57168170 +.00000000 +00000-0 +00000-0 0 00003
2 39078 0.0239 127.1365 0001322 315.6407 305.1898 1.00270721 06
| Epoch (UTC): | 25 May 2026 13:43:13 |
| Eccentricity: | 0.0001322 |
| inclination: | 0.0239° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 127.1365° |
| argument of perigee: | 315.6407° |
| revolutions per day: | 1.00270721 |
| mean anomaly at epoch: | 305.1898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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