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 23159.51520074 .00001064 00000-0 10122-3 0 9995
2 28414 97.6921 178.7353 0004784 309.3268 50.7528 14.95517350 21148
| Epoch (UTC): | 08 June 2023 12:21:53 |
| Eccentricity: | 0.0004784 |
| inclination: | 97.6921° |
| perigee height: | 577 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 178.7353° |
| argument of perigee: | 309.3268° |
| revolutions per day: | 14.95517350 |
| mean anomaly at epoch: | 50.7528° |
| orbit number at epoch: | 2114 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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