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 41845U 16066E 23108.25374105 .09688058 49398+0 20392-1 0 9995
2 41845 98.7320 280.7458 0014497 235.4097 246.7034 16.09018510342480
| Epoch (UTC): | 18 April 2023 06:05:23 |
| Eccentricity: | 0.0014497 |
| inclination: | 98.7320° |
| perigee height: | 240 km |
| apogee height: | 259 km |
| right ascension of ascending node: | 280.7458° |
| argument of perigee: | 235.4097° |
| revolutions per day: | 16.09018510 |
| mean anomaly at epoch: | 246.7034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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