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 26032U 26150.42007634 +.00000000 +00000-0 +21897-3 0 00006
2 26032 98.3019 321.6564 0003185 341.2449 18.8642 14.76684890 08
| Epoch (UTC): | 30 May 2026 10:04:54 |
| Eccentricity: | 0.0003185 |
| inclination: | 98.3019° |
| perigee height: | 638 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 321.6564° |
| argument of perigee: | 341.2449° |
| revolutions per day: | 14.76684890 |
| mean anomaly at epoch: | 18.8642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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