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 04320U 26031.87395500 +.00000000 +00000-0 +15722-3 0 00001
2 04320 101.3907 71.2668 0028098 219.0109 314.7032 12.52119541 02
| Epoch (UTC): | 31 January 2026 20:58:29 |
| Eccentricity: | 0.0028098 |
| inclination: | 101.3907° |
| perigee height: | 1434 km |
| apogee height: | 1478 km |
| right ascension of ascending node: | 71.2668° |
| argument of perigee: | 219.0109° |
| revolutions per day: | 12.52119541 |
| mean anomaly at epoch: | 314.7032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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