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 43034U 26145.63937292 +.00000000 +00000-0 +26988-3 0 00002
2 43034 97.1003 181.0729 0001583 105.3754 254.7659 15.23589838 06
| Epoch (UTC): | 25 May 2026 15:20:41 |
| Eccentricity: | 0.0001583 |
| inclination: | 97.1003° |
| perigee height: | 494 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 181.0729° |
| argument of perigee: | 105.3754° |
| revolutions per day: | 15.23589838 |
| mean anomaly at epoch: | 254.7659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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