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 41619U 16040W 23266.20301408 .10242607 23765-5 10219-2 0 9994
2 41619 97.1197 318.8504 0010645 257.6025 102.4083 16.38035722392312
| Epoch (UTC): | 23 September 2023 04:52:20 |
| Eccentricity: | 0.0010645 |
| inclination: | 97.1197° |
| perigee height: | 164 km |
| apogee height: | 178 km |
| right ascension of ascending node: | 318.8504° |
| argument of perigee: | 257.6025° |
| revolutions per day: | 16.38035722 |
| mean anomaly at epoch: | 102.4083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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