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 62787U 26145.57936399 +.00000000 +00000-0 +14287-3 0 00007
2 62787 88.9738 86.2158 0003033 68.0859 292.0615 13.51012559 07
| Epoch (UTC): | 25 May 2026 13:54:17 |
| Eccentricity: | 0.0003033 |
| inclination: | 88.9738° |
| perigee height: | 1066 km |
| apogee height: | 1071 km |
| right ascension of ascending node: | 86.2158° |
| argument of perigee: | 68.0859° |
| revolutions per day: | 13.51012559 |
| mean anomaly at epoch: | 292.0615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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