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 43803U 26145.58022645 +.00000000 +00000-0 +52678-3 0 00002
2 43803 97.4147 208.3482 0005046 8.6657 351.4671 15.32822128 07
| Epoch (UTC): | 25 May 2026 13:55:31 |
| Eccentricity: | 0.0005046 |
| inclination: | 97.4147° |
| perigee height: | 464 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 208.3482° |
| argument of perigee: | 8.6657° |
| revolutions per day: | 15.32822128 |
| mean anomaly at epoch: | 351.4671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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