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 is defined by the following mean orbital elements,
1 42941U 17056A 25165.47189940 0.00000000 00000-0 00000-0 0 03
2 42941 62.9040 184.1614 6740770 269.2380 90.7620 2.00591119 01
| Epoch (UTC): | 14 June 2025 11:19:32 |
| Eccentricity: | 0.6740770 |
| inclination: | 62.9040° |
| perigee height: | 2277 km |
| apogee height: | 38081 km |
| right ascension of ascending node: | 184.1614° |
| argument of perigee: | 269.2380° |
| revolutions per day: | 2.00591119 |
| mean anomaly at epoch: | 90.7620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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