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 62154U 26145.23828163 +.00000000 +00000-0 +10587-2 0 00005
2 62154 43.0030 86.0956 0001516 271.9670 88.1008 15.27593935 03
| Epoch (UTC): | 25 May 2026 05:43:07 |
| Eccentricity: | 0.0001516 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 86.0956° |
| argument of perigee: | 271.9670° |
| revolutions per day: | 15.27593935 |
| mean anomaly at epoch: | 88.1008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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