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 28414U 04035B 23151.88765197 .00000857 00000-0 82533-4 0 9999
2 28414 97.6929 171.2465 0005367 341.6387 18.4639 14.95502765 20009
| Epoch (UTC): | 31 May 2023 21:18:13 |
| Eccentricity: | 0.0005367 |
| inclination: | 97.6929° |
| perigee height: | 577 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 171.2465° |
| argument of perigee: | 341.6387° |
| revolutions per day: | 14.95502765 |
| mean anomaly at epoch: | 18.4639° |
| orbit number at epoch: | 2000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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