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 40043U 26069.93783078 +.00000000 +00000-0 +29159-3 0 00001
2 40043 97.7677 222.3049 0050264 38.2979 322.1788 14.84736182 08
| Epoch (UTC): | 10 March 2026 22:30:28 |
| Eccentricity: | 0.0050264 |
| inclination: | 97.7677° |
| perigee height: | 579 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 222.3049° |
| argument of perigee: | 38.2979° |
| revolutions per day: | 14.84736182 |
| mean anomaly at epoch: | 322.1788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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