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 26111.42780535 +.00000000 +00000-0 +54394-3 0 00004
2 43803 97.4168 174.1327 0007531 112.4689 247.7350 15.31830017 04
| Epoch (UTC): | 21 April 2026 10:16:02 |
| Eccentricity: | 0.0007531 |
| inclination: | 97.4168° |
| perigee height: | 465 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 174.1327° |
| argument of perigee: | 112.4689° |
| revolutions per day: | 15.31830017 |
| mean anomaly at epoch: | 247.7350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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