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 43805U 26050.13864936 +.00000000 +00000-0 +10635-2 0 00003
2 43805 97.4152 125.0110 0003863 265.7074 94.3743 15.62703609 00
| Epoch (UTC): | 19 February 2026 03:19:39 |
| Eccentricity: | 0.0003863 |
| inclination: | 97.4152° |
| perigee height: | 377 km |
| apogee height: | 382 km |
| right ascension of ascending node: | 125.0110° |
| argument of perigee: | 265.7074° |
| revolutions per day: | 15.62703609 |
| mean anomaly at epoch: | 94.3743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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