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 36828U 26150.45354991 +.00000000 +00000-0 +00000-0 0 00004
2 36828 54.2994 163.1194 0058769 225.1266 130.5780 1.00277601 04
| Epoch (UTC): | 30 May 2026 10:53:06 |
| Eccentricity: | 0.0058769 |
| inclination: | 54.2994° |
| perigee height: | 35537 km |
| apogee height: | 36033 km |
| right ascension of ascending node: | 163.1194° |
| argument of perigee: | 225.1266° |
| revolutions per day: | 1.00277601 |
| mean anomaly at epoch: | 130.5780° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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