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 32294U 26145.51739174 +.00000000 +00000-0 +00000-0 0 00008
2 32294 5.1961 73.7679 0003898 345.1066 35.5938 1.00269130 01
| Epoch (UTC): | 25 May 2026 12:25:02 |
| Eccentricity: | 0.0003898 |
| inclination: | 5.1961° |
| perigee height: | 35771 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 73.7679° |
| argument of perigee: | 345.1066° |
| revolutions per day: | 1.00269130 |
| mean anomaly at epoch: | 35.5938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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