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 44450U 26145.36166631 +.00000000 +00000-0 +17101-3 0 00003
2 44450 34.9916 108.7372 0009359 237.4114 122.5690 15.02561477 00
| Epoch (UTC): | 25 May 2026 08:40:47 |
| Eccentricity: | 0.0009359 |
| inclination: | 34.9916° |
| perigee height: | 553 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 108.7372° |
| argument of perigee: | 237.4114° |
| revolutions per day: | 15.02561477 |
| mean anomaly at epoch: | 122.5690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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