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 44009U 26065.99824301 +.00000000 +00000-0 +00000-0 0 00005
2 44009 20.8449 118.4113 4988644 213.7539 101.1463 1.91639976 05
| Epoch (UTC): | 06 March 2026 23:57:28 |
| Eccentricity: | 0.4988644 |
| inclination: | 20.8449° |
| perigee height: | 7342 km |
| apogee height: | 34659 km |
| right ascension of ascending node: | 118.4113° |
| argument of perigee: | 213.7539° |
| revolutions per day: | 1.91639976 |
| mean anomaly at epoch: | 101.1463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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