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 41923U 17003G 23150.22206335 .00000258 00000-0 85029-4 0 9997
2 41923 86.4011 193.9298 0002062 91.1541 268.9891 14.34218355333584
| Epoch (UTC): | 30 May 2023 05:19:46 |
| Eccentricity: | 0.0002062 |
| inclination: | 86.4011° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.9298° |
| argument of perigee: | 91.1541° |
| revolutions per day: | 14.34218355 |
| mean anomaly at epoch: | 268.9891° |
| orbit number at epoch: | 33358 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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