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 44312U 26145.39909215 +.00000000 +00000-0 +38889-3 0 00002
2 44312 44.9737 122.3015 0004594 185.9851 174.0979 15.32051118 07
| Epoch (UTC): | 25 May 2026 09:34:41 |
| Eccentricity: | 0.0004594 |
| inclination: | 44.9737° |
| perigee height: | 467 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 122.3015° |
| argument of perigee: | 185.9851° |
| revolutions per day: | 15.32051118 |
| mean anomaly at epoch: | 174.0979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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