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 62183U 26145.22148166 +.00000000 +00000-0 +13328-3 0 00001
2 62183 70.0015 331.6967 0002688 265.8713 94.2139 14.98332920 05
| Epoch (UTC): | 25 May 2026 05:18:56 |
| Eccentricity: | 0.0002688 |
| inclination: | 70.0015° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.6967° |
| argument of perigee: | 265.8713° |
| revolutions per day: | 14.98332920 |
| mean anomaly at epoch: | 94.2139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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