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 62902U 26144.72869698 +.00000000 +00000-0 +10922-3 0 00001
2 62902 81.9948 98.4316 0011227 127.9003 232.3234 14.94925952 05
| Epoch (UTC): | 24 May 2026 17:29:19 |
| Eccentricity: | 0.0011227 |
| inclination: | 81.9948° |
| perigee height: | 575 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 98.4316° |
| argument of perigee: | 127.9003° |
| revolutions per day: | 14.94925952 |
| mean anomaly at epoch: | 232.3234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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