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 43796U 26145.64106301 +.00000000 +00000-0 +51018-3 0 00009
2 43796 97.4454 215.1271 0007104 18.4267 341.7231 15.34132015 09
| Epoch (UTC): | 25 May 2026 15:23:07 |
| Eccentricity: | 0.0007104 |
| inclination: | 97.4454° |
| perigee height: | 459 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 215.1271° |
| argument of perigee: | 18.4267° |
| revolutions per day: | 15.34132015 |
| mean anomaly at epoch: | 341.7231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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