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 23190U 94045B 23150.28401583 -.00000008 00000-0 15579-4 0 9999
2 23190 74.0287 101.3122 0019867 310.7329 49.2065 13.74173735445461
| Epoch (UTC): | 30 May 2023 06:48:58 |
| Eccentricity: | 0.0019867 |
| inclination: | 74.0287° |
| perigee height: | 970 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 101.3122° |
| argument of perigee: | 310.7329° |
| revolutions per day: | 13.74173735 |
| mean anomaly at epoch: | 49.2065° |
| orbit number at epoch: | 44546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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