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 26129.63175824 +.00000000 +00000-0 +57538-3 0 00002
2 00011 32.8690 231.0710 1444593 197.4993 157.0300 11.90414802 04
| Epoch (UTC): | 09 May 2026 15:09:43 |
| Eccentricity: | 0.1444593 |
| inclination: | 32.8690° |
| perigee height: | 554 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 231.0710° |
| argument of perigee: | 197.4993° |
| revolutions per day: | 11.90414802 |
| mean anomaly at epoch: | 157.0300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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