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 36831U 26145.37044388 +.00000000 +00000-0 +00000-0 0 00009
2 36831 0.0007 34.9680 0006719 29.0749 315.1815 1.00270686 08
| Epoch (UTC): | 25 May 2026 08:53:26 |
| Eccentricity: | 0.0006719 |
| inclination: | 0.0007° |
| perigee height: | 35759 km |
| apogee height: | 35815 km |
| right ascension of ascending node: | 34.9680° |
| argument of perigee: | 29.0749° |
| revolutions per day: | 1.00270686 |
| mean anomaly at epoch: | 315.1815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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