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 40024U 26072.51845422 +.00000000 +00000-0 +75539-3 0 00003
2 40024 98.0842 96.6153 0004981 139.6908 220.4700 15.28283055 05
| Epoch (UTC): | 13 March 2026 12:26:34 |
| Eccentricity: | 0.0004981 |
| inclination: | 98.0842° |
| perigee height: | 478 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.6153° |
| argument of perigee: | 139.6908° |
| revolutions per day: | 15.28283055 |
| mean anomaly at epoch: | 220.4700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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