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 26546U 26155.12434212 +.00000000 +00000-0 +27623-3 0 00007
2 26546 64.5494 110.9700 0041822 285.3645 74.2853 15.05416397 05
| Epoch (UTC): | 04 June 2026 02:59:03 |
| Eccentricity: | 0.0041822 |
| inclination: | 64.5494° |
| perigee height: | 521 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 110.9700° |
| argument of perigee: | 285.3645° |
| revolutions per day: | 15.05416397 |
| mean anomaly at epoch: | 74.2853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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