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 26139.11698419 +.00000000 +00000-0 +37434-3 0 00005
2 43803 97.4142 201.8701 0005752 31.4913 328.6673 15.32643998 01
| Epoch (UTC): | 19 May 2026 02:48:27 |
| Eccentricity: | 0.0005752 |
| inclination: | 97.4142° |
| perigee height: | 464 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 201.8701° |
| argument of perigee: | 31.4913° |
| revolutions per day: | 15.32643998 |
| mean anomaly at epoch: | 328.6673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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