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 40545U 15017B 25197.35538010 -.00000077 00000-0 00000-0 0 9996
2 40545 56.8903 350.7658 0002685 226.6603 133.3188 1.70475580 26520
| Epoch (UTC): | 16 July 2025 08:31:44 |
| Eccentricity: | 0.0002685 |
| inclination: | 56.8903° |
| perigee height: | 23214 km |
| apogee height: | 23230 km |
| right ascension of ascending node: | 350.7658° |
| argument of perigee: | 226.6603° |
| revolutions per day: | 1.70475580 |
| mean anomaly at epoch: | 133.3188° |
| orbit number at epoch: | 2652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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