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 26053.15631799 +.00000000 +00000-0 +27771-3 0 00008
2 40043 97.7646 205.9528 0050995 92.2241 268.4815 14.84631091 02
| Epoch (UTC): | 22 February 2026 03:45:05 |
| Eccentricity: | 0.0050995 |
| inclination: | 97.7646° |
| perigee height: | 579 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 205.9528° |
| argument of perigee: | 92.2241° |
| revolutions per day: | 14.84631091 |
| mean anomaly at epoch: | 268.4815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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