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 data is extracted from the following two-line orbital elements,
1 40900U 15049B 23087.78616407 .08306610 24723-5 22534-2 0 9996
2 40900 97.3422 117.7994 0007846 241.5351 216.5981 16.28124363418658
| Epoch (UTC): | 28 March 2023 18:52:04 |
| Eccentricity: | 0.0007846 |
| inclination: | 97.3422° |
| perigee height: | 192 km |
| apogee height: | 203 km |
| right ascension of ascending node: | 117.7994° |
| argument of perigee: | 241.5351° |
| revolutions per day: | 16.28124363 |
| mean anomaly at epoch: | 216.5981° |
| orbit number at epoch: | 41865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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