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 23154.56578079 .00000048 00000-0 48549-4 0 9992
2 25407 71.0098 145.3662 0005780 138.2824 221.8741 14.15917492284103
| Epoch (UTC): | 03 June 2023 13:34:43 |
| Eccentricity: | 0.0005780 |
| inclination: | 71.0098° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 145.3662° |
| argument of perigee: | 138.2824° |
| revolutions per day: | 14.15917492 |
| mean anomaly at epoch: | 221.8741° |
| orbit number at epoch: | 28410 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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