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 40926U 15051B 21057.93770894 .05243455 22735-5 10757-2 0 9999
2 40926 97.0197 120.9742 0006610 258.8279 223.7215 16.31196197307135
| Epoch (UTC): | 26 February 2021 22:30:18 |
| Eccentricity: | 0.0006610 |
| inclination: | 97.0197° |
| perigee height: | 185 km |
| apogee height: | 193 km |
| right ascension of ascending node: | 120.9742° |
| argument of perigee: | 258.8279° |
| revolutions per day: | 16.31196197 |
| mean anomaly at epoch: | 223.7215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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