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 58989U 26145.41041065 +.00000000 +00000-0 +18180-3 0 00002
2 58989 97.9977 204.1104 0004227 204.3482 155.7526 14.72396561 04
| Epoch (UTC): | 25 May 2026 09:50:59 |
| Eccentricity: | 0.0004227 |
| inclination: | 97.9977° |
| perigee height: | 650 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 204.1104° |
| argument of perigee: | 204.3482° |
| revolutions per day: | 14.72396561 |
| mean anomaly at epoch: | 155.7526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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