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 43880U 26106.71974515 +.00000000 +00000-0 +41496-3 0 00007
2 43880 97.5863 32.4646 0008586 167.3462 192.8002 15.42477857 06
| Epoch (UTC): | 16 April 2026 17:16:25 |
| Eccentricity: | 0.0008586 |
| inclination: | 97.5863° |
| perigee height: | 433 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 32.4646° |
| argument of perigee: | 167.3462° |
| revolutions per day: | 15.42477857 |
| mean anomaly at epoch: | 192.8002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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