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 43609U 26145.64065632 +.00000000 +00000-0 +11167-3 0 00004
2 43609 98.5191 218.2740 0011333 155.7120 204.4601 14.34171478 00
| Epoch (UTC): | 25 May 2026 15:22:32 |
| Eccentricity: | 0.0011333 |
| inclination: | 98.5191° |
| perigee height: | 770 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 218.2740° |
| argument of perigee: | 155.7120° |
| revolutions per day: | 14.34171478 |
| mean anomaly at epoch: | 204.4601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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