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 59272U 26145.50172720 +.00000000 +00000-0 +38508-5 0 00009
2 59272 53.1596 183.8725 0001153 81.8153 278.2979 15.30190792 07
| Epoch (UTC): | 25 May 2026 12:02:29 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 183.8725° |
| argument of perigee: | 81.8153° |
| revolutions per day: | 15.30190792 |
| mean anomaly at epoch: | 278.2979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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