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 26050.16428990 +.00000000 +00000-0 +32716-3 0 00009
2 00020 33.3444 331.8604 1638082 140.8523 232.2820 11.61831501 07
| Epoch (UTC): | 19 February 2026 03:56:34 |
| Eccentricity: | 0.1638082 |
| inclination: | 33.3444° |
| perigee height: | 508 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 331.8604° |
| argument of perigee: | 140.8523° |
| revolutions per day: | 11.61831501 |
| mean anomaly at epoch: | 232.2820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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