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 44451U 26145.33821608 +.00000000 +00000-0 +17956-3 0 00001
2 44451 34.9927 108.7595 0000920 241.4227 118.6389 15.02548271 03
| Epoch (UTC): | 25 May 2026 08:07:01 |
| Eccentricity: | 0.0000920 |
| inclination: | 34.9927° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 108.7595° |
| argument of perigee: | 241.4227° |
| revolutions per day: | 15.02548271 |
| mean anomaly at epoch: | 118.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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