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 59224U 26145.58596899 +.00000000 +00000-0 +37266-3 0 00009
2 59224 97.6614 120.9369 0014689 134.7379 225.5054 15.18947508 00
| Epoch (UTC): | 25 May 2026 14:03:47 |
| Eccentricity: | 0.0014689 |
| inclination: | 97.6614° |
| perigee height: | 499 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 120.9369° |
| argument of perigee: | 134.7379° |
| revolutions per day: | 15.18947508 |
| mean anomaly at epoch: | 225.5054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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