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 58974U 26145.43415956 +.00000000 +00000-0 +49194-4 0 00002
2 58974 53.1612 300.1811 0001122 89.7734 270.3395 15.30196381 07
| Epoch (UTC): | 25 May 2026 10:25:11 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.1811° |
| argument of perigee: | 89.7734° |
| revolutions per day: | 15.30196381 |
| mean anomaly at epoch: | 270.3395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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