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 00011U 26131.64441571 +.00000000 +00000-0 +47159-3 0 00009
2 00011 32.8703 223.4542 1444754 208.9538 142.2791 11.90418566 00
| Epoch (UTC): | 11 May 2026 15:27:57 |
| Eccentricity: | 0.1444754 |
| inclination: | 32.8703° |
| perigee height: | 553 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 223.4542° |
| argument of perigee: | 208.9538° |
| revolutions per day: | 11.90418566 |
| mean anomaly at epoch: | 142.2791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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