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 62781U 26145.48534612 +.00000000 +00000-0 +72344-3 0 00001
2 62781 53.1598 323.2171 0001469 98.4852 261.6318 15.34406883 01
| Epoch (UTC): | 25 May 2026 11:38:53 |
| Eccentricity: | 0.0001469 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 323.2171° |
| argument of perigee: | 98.4852° |
| revolutions per day: | 15.34406883 |
| mean anomaly at epoch: | 261.6318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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