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 23152.17558026 .00000292 00000-0 97353-4 0 9991
2 41923 86.4009 193.1147 0002065 91.5329 268.6103 14.34219503333867
| Epoch (UTC): | 01 June 2023 04:12:50 |
| Eccentricity: | 0.0002065 |
| inclination: | 86.4009° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 193.1147° |
| argument of perigee: | 91.5329° |
| revolutions per day: | 14.34219503 |
| mean anomaly at epoch: | 268.6103° |
| orbit number at epoch: | 33386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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