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 62514U 26144.88852630 +.00000000 +00000-0 +14978-2 0 00009
2 62514 43.0014 331.3378 0002264 278.2628 81.7983 15.70841502 08
| Epoch (UTC): | 24 May 2026 21:19:28 |
| Eccentricity: | 0.0002264 |
| inclination: | 43.0014° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 331.3378° |
| argument of perigee: | 278.2628° |
| revolutions per day: | 15.70841502 |
| mean anomaly at epoch: | 81.7983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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