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 62774U 26145.52580251 +.00000000 +00000-0 +65090-3 0 00008
2 62774 53.1599 324.9564 0001105 87.9860 272.1269 15.34408075 04
| Epoch (UTC): | 25 May 2026 12:37:09 |
| Eccentricity: | 0.0001105 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 324.9564° |
| argument of perigee: | 87.9860° |
| revolutions per day: | 15.34408075 |
| mean anomaly at epoch: | 272.1269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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