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 00309U 26153.63661475 +.00000000 +00000-0 +12235-3 0 00006
2 00309 58.0911 273.2167 0177639 245.3622 112.8815 14.60647566 04
| Epoch (UTC): | 02 June 2026 15:16:43 |
| Eccentricity: | 0.0177639 |
| inclination: | 58.0911° |
| perigee height: | 566 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 273.2167° |
| argument of perigee: | 245.3622° |
| revolutions per day: | 14.60647566 |
| mean anomaly at epoch: | 112.8815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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