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 62519U 26145.53937278 +.00000000 +00000-0 +22532-2 0 00004
2 62519 42.9985 327.6240 0001533 261.5027 98.5667 15.70814986 01
| Epoch (UTC): | 25 May 2026 12:56:41 |
| Eccentricity: | 0.0001533 |
| inclination: | 42.9985° |
| perigee height: | 356 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 327.6240° |
| argument of perigee: | 261.5027° |
| revolutions per day: | 15.70814986 |
| mean anomaly at epoch: | 98.5667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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