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 40018U 14033J 25137.80799339 .00000870 00000-0 13698-3 0 9995
2 40018 97.8510 277.2478 0067760 32.6646 327.8726 14.73445027585320
| Epoch (UTC): | 17 May 2025 19:23:30 |
| Eccentricity: | 0.0067760 |
| inclination: | 97.8510° |
| perigee height: | 602 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 277.2478° |
| argument of perigee: | 32.6646° |
| revolutions per day: | 14.73445027 |
| mean anomaly at epoch: | 327.8726° |
| orbit number at epoch: | 58532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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