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 25942U 26100.17446904 +.00000000 +00000-0 +12497-3 0 00005
2 25942 98.7292 151.3664 0096693 58.9809 302.0829 14.38376529 01
| Epoch (UTC): | 10 April 2026 04:11:14 |
| Eccentricity: | 0.0096693 |
| inclination: | 98.7292° |
| perigee height: | 695 km |
| apogee height: | 833 km |
| right ascension of ascending node: | 151.3664° |
| argument of perigee: | 58.9809° |
| revolutions per day: | 14.38376529 |
| mean anomaly at epoch: | 302.0829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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