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 42075U 17016A 25073.40952106 -.00000103 00000-0 00000-0 0 9992
2 42075 0.0265 174.8880 0000643 154.1916 338.6295 1.00269119 29285
| Epoch (UTC): | 14 March 2025 09:49:42 |
| Eccentricity: | 0.0000643 |
| inclination: | 0.0265° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 174.8880° |
| argument of perigee: | 154.1916° |
| revolutions per day: | 1.00269119 |
| mean anomaly at epoch: | 338.6295° |
| orbit number at epoch: | 2928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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