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 43804U 26141.29248296 +.00000000 +00000-0 +32074-3 0 00007
2 43804 97.4201 201.7974 0010216 25.7327 334.4419 15.27719373 03
| Epoch (UTC): | 21 May 2026 07:01:10 |
| Eccentricity: | 0.0010216 |
| inclination: | 97.4201° |
| perigee height: | 476 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 201.7974° |
| argument of perigee: | 25.7327° |
| revolutions per day: | 15.27719373 |
| mean anomaly at epoch: | 334.4419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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