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 26549U 26155.15799927 +.00000000 +00000-0 +15384-3 0 00001
2 26549 64.5494 36.1312 0042871 311.0656 48.6753 14.91137493 05
| Epoch (UTC): | 04 June 2026 03:47:31 |
| Eccentricity: | 0.0042871 |
| inclination: | 64.5494° |
| perigee height: | 564 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 36.1312° |
| argument of perigee: | 311.0656° |
| revolutions per day: | 14.91137493 |
| mean anomaly at epoch: | 48.6753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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