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 43758U 26050.19349644 +.00000000 +00000-0 +69023-3 0 00006
2 43758 97.4668 123.6621 0007781 335.0760 25.0108 15.39016308 09
| Epoch (UTC): | 19 February 2026 04:38:38 |
| Eccentricity: | 0.0007781 |
| inclination: | 97.4668° |
| perigee height: | 444 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 123.6621° |
| argument of perigee: | 335.0760° |
| revolutions per day: | 15.39016308 |
| mean anomaly at epoch: | 25.0108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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