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 59121U 26145.37862560 +.00000000 +00000-0 +18172-3 0 00008
2 59121 97.5603 282.4538 0010153 335.2350 24.8402 15.30435472 07
| Epoch (UTC): | 25 May 2026 09:05:13 |
| Eccentricity: | 0.0010153 |
| inclination: | 97.5603° |
| perigee height: | 468 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 282.4538° |
| argument of perigee: | 335.2350° |
| revolutions per day: | 15.30435472 |
| mean anomaly at epoch: | 24.8402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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