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 62169U 26145.26335904 +.00000000 +00000-0 +23894-3 0 00006
2 62169 70.0019 331.4377 0002657 267.6209 92.4646 14.98336171 07
| Epoch (UTC): | 25 May 2026 06:19:14 |
| Eccentricity: | 0.0002657 |
| inclination: | 70.0019° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.4377° |
| argument of perigee: | 267.6209° |
| revolutions per day: | 14.98336171 |
| mean anomaly at epoch: | 92.4646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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