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 62170U 26144.94208168 +.00000000 +00000-0 +24273-3 0 00005
2 62170 70.0018 332.3268 0002687 267.4844 92.6008 14.98337375 04
| Epoch (UTC): | 24 May 2026 22:36:35 |
| Eccentricity: | 0.0002687 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 332.3268° |
| argument of perigee: | 267.4844° |
| revolutions per day: | 14.98337375 |
| mean anomaly at epoch: | 92.6008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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