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 25399U 98043F 23083.12821548 .00000358 00000-0 17262-3 0 9996
2 25399 98.8213 36.9612 0000785 309.8898 50.2212 14.24863878284123
| Epoch (UTC): | 24 March 2023 03:04:37 |
| Eccentricity: | 0.0000785 |
| inclination: | 98.8213° |
| perigee height: | 808 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 36.9612° |
| argument of perigee: | 309.8898° |
| revolutions per day: | 14.24863878 |
| mean anomaly at epoch: | 50.2212° |
| orbit number at epoch: | 28412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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