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 23155.41354094 .00000003 00000-0 25768-4 0 9995
2 25407 71.0098 143.5841 0005705 136.9332 223.2238 14.15917653284227
| Epoch (UTC): | 04 June 2023 09:55:29 |
| Eccentricity: | 0.0005705 |
| inclination: | 71.0098° |
| perigee height: | 835 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 143.5841° |
| argument of perigee: | 136.9332° |
| revolutions per day: | 14.15917653 |
| mean anomaly at epoch: | 223.2238° |
| orbit number at epoch: | 28422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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