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 59207U 26145.30664340 +.00000000 +00000-0 +11723-5 0 00009
2 59207 53.1594 158.4963 0000948 82.0609 278.0502 15.34397799 05
| Epoch (UTC): | 25 May 2026 07:21:33 |
| Eccentricity: | 0.0000948 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 158.4963° |
| argument of perigee: | 82.0609° |
| revolutions per day: | 15.34397799 |
| mean anomaly at epoch: | 278.0502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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