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 44547U 26145.50417661 +.00000000 +00000-0 +11481-3 0 00003
2 44547 98.4125 156.6106 0004967 211.0333 149.0558 14.32689054 03
| Epoch (UTC): | 25 May 2026 12:06:00 |
| Eccentricity: | 0.0004967 |
| inclination: | 98.4125° |
| perigee height: | 779 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 156.6106° |
| argument of perigee: | 211.0333° |
| revolutions per day: | 14.32689054 |
| mean anomaly at epoch: | 149.0558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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