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 23151.45732526 .00000235 00000-0 14374-3 0 9992
2 25407 71.0095 151.9004 0005973 143.9820 216.1706 14.15916343283938
| Epoch (UTC): | 31 May 2023 10:58:32 |
| Eccentricity: | 0.0005973 |
| inclination: | 71.0095° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 151.9004° |
| argument of perigee: | 143.9820° |
| revolutions per day: | 14.15916343 |
| mean anomaly at epoch: | 216.1706° |
| orbit number at epoch: | 28393 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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