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 62915U 26145.59084660 +.00000000 +00000-0 +16968-2 0 00004
2 62915 43.0032 244.3957 0003054 268.4596 91.5922 15.70892248 07
| Epoch (UTC): | 25 May 2026 14:10:49 |
| Eccentricity: | 0.0003054 |
| inclination: | 43.0032° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 244.3957° |
| argument of perigee: | 268.4596° |
| revolutions per day: | 15.70892248 |
| mean anomaly at epoch: | 91.5922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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