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 62137U 26145.48451181 +.00000000 +00000-0 +69505-3 0 00000
2 62137 43.0009 62.4892 0000649 269.0692 91.0085 15.27590713 04
| Epoch (UTC): | 25 May 2026 11:37:41 |
| Eccentricity: | 0.0000649 |
| inclination: | 43.0009° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 62.4892° |
| argument of perigee: | 269.0692° |
| revolutions per day: | 15.27590713 |
| mean anomaly at epoch: | 91.0085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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