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 44520U 26114.96522890 +.00000000 +00000-0 +71716-4 0 00009
2 44520 97.7794 128.5658 0010697 155.9941 204.1782 14.96523813 08
| Epoch (UTC): | 24 April 2026 23:09:55 |
| Eccentricity: | 0.0010697 |
| inclination: | 97.7794° |
| perigee height: | 570 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 128.5658° |
| argument of perigee: | 155.9941° |
| revolutions per day: | 14.96523813 |
| mean anomaly at epoch: | 204.1782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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