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 42830U 17042F 25015.79437342 .16566363 23380-5 13045-2 0 9995
2 42830 97.3125 220.4047 0007235 314.2941 45.7764 16.40208236410815
| Epoch (UTC): | 15 January 2025 19:03:53 |
| Eccentricity: | 0.0007235 |
| inclination: | 97.3125° |
| perigee height: | 160 km |
| apogee height: | 170 km |
| right ascension of ascending node: | 220.4047° |
| argument of perigee: | 314.2941° |
| revolutions per day: | 16.40208236 |
| mean anomaly at epoch: | 45.7764° |
| orbit number at epoch: | 41081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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