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 23159.36975538 -.00000145 00000-0 -49587-4 0 9999
2 25407 71.0098 135.2681 0005504 129.1415 231.0198 14.15917584284786
| Epoch (UTC): | 08 June 2023 08:52:26 |
| Eccentricity: | 0.0005504 |
| inclination: | 71.0098° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 135.2681° |
| argument of perigee: | 129.1415° |
| revolutions per day: | 14.15917584 |
| mean anomaly at epoch: | 231.0198° |
| orbit number at epoch: | 28478 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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