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 63692U 26145.63220657 +.00000000 +00000-0 +45083-4 0 00002
2 63692 86.5014 320.6362 0001511 82.4006 277.7300 13.24407804 01
| Epoch (UTC): | 25 May 2026 15:10:22 |
| Eccentricity: | 0.0001511 |
| inclination: | 86.5014° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 320.6362° |
| argument of perigee: | 82.4006° |
| revolutions per day: | 13.24407804 |
| mean anomaly at epoch: | 277.7300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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