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 20509U 90017B 25194.02503082 .00000060 00000-0 45831-4 0 9995
2 20509 82.9549 302.2783 0042392 206.6540 153.2438 13.75840404775600
| Epoch (UTC): | 13 July 2025 00:36:02 |
| Eccentricity: | 0.0042392 |
| inclination: | 82.9549° |
| perigee height: | 947 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 302.2783° |
| argument of perigee: | 206.6540° |
| revolutions per day: | 13.75840404 |
| mean anomaly at epoch: | 153.2438° |
| orbit number at epoch: | 77560 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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