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 62092U 26145.44318733 +.00000000 +00000-0 +15903-2 0 00003
2 62092 42.9971 300.5049 0000058 277.3084 82.7777 15.70973249 03
| Epoch (UTC): | 25 May 2026 10:38:11 |
| Eccentricity: | 0.0000058 |
| inclination: | 42.9971° |
| perigee height: | 356 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 300.5049° |
| argument of perigee: | 277.3084° |
| revolutions per day: | 15.70973249 |
| mean anomaly at epoch: | 82.7777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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