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 25407U 98045B 23151.95185250 .00000211 00000-0 13137-3 0 9993
2 25407 71.0096 150.8609 0005939 143.0583 217.0950 14.15916607283739
| Epoch (UTC): | 31 May 2023 22:50:40 |
| Eccentricity: | 0.0005939 |
| inclination: | 71.0096° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 150.8609° |
| argument of perigee: | 143.0583° |
| revolutions per day: | 14.15916607 |
| mean anomaly at epoch: | 217.0950° |
| orbit number at epoch: | 28373 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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