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 31118U 07012B 25137.43376923 .00000503 00000-0 89978-4 0 9992
2 31118 98.0978 83.9627 0015843 50.1497 310.1101 14.71028526969613
| Epoch (UTC): | 17 May 2025 10:24:37 |
| Eccentricity: | 0.0015843 |
| inclination: | 98.0978° |
| perigee height: | 646 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 83.9627° |
| argument of perigee: | 50.1497° |
| revolutions per day: | 14.71028526 |
| mean anomaly at epoch: | 310.1101° |
| orbit number at epoch: | 96961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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