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 26050.21292640 +.00000000 +00000-0 +68953-3 0 00009
2 43880 97.5863 333.8511 0010858 41.7555 318.4516 15.38661155 05
| Epoch (UTC): | 19 February 2026 05:06:36 |
| Eccentricity: | 0.0010858 |
| inclination: | 97.5863° |
| perigee height: | 443 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 333.8511° |
| argument of perigee: | 41.7555° |
| revolutions per day: | 15.38661155 |
| mean anomaly at epoch: | 318.4516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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