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 05732U 26129.76854580 +.00000000 +00000-0 +93308-7 0 00003
2 05732 81.2532 224.4016 0049826 267.7407 91.8056 14.06427126 03
| Epoch (UTC): | 09 May 2026 18:26:42 |
| Eccentricity: | 0.0049826 |
| inclination: | 81.2532° |
| perigee height: | 836 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 224.4016° |
| argument of perigee: | 267.7407° |
| revolutions per day: | 14.06427126 |
| mean anomaly at epoch: | 91.8056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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