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 43011U 26145.61993051 +.00000000 +00000-0 +83294-4 0 00004
2 43011 98.9563 163.5243 0009192 214.4229 145.6357 14.28781075 04
| Epoch (UTC): | 25 May 2026 14:52:41 |
| Eccentricity: | 0.0009192 |
| inclination: | 98.9563° |
| perigee height: | 789 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 163.5243° |
| argument of perigee: | 214.4229° |
| revolutions per day: | 14.28781075 |
| mean anomaly at epoch: | 145.6357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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