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 00020U 26046.12514747 +.00000000 +00000-0 +34413-3 0 00002
2 00020 33.3447 346.4009 1638215 119.1980 258.2325 11.61823803 09
| Epoch (UTC): | 15 February 2026 03:00:12 |
| Eccentricity: | 0.1638215 |
| inclination: | 33.3447° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 346.4009° |
| argument of perigee: | 119.1980° |
| revolutions per day: | 11.61823803 |
| mean anomaly at epoch: | 258.2325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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