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 15890U 26064.67110565 +.00000000 +00000-0 +85053-4 0 00000
2 15890 82.5284 158.7286 0020791 151.6567 208.5786 14.85776438 00
| Epoch (UTC): | 05 March 2026 16:06:23 |
| Eccentricity: | 0.0020791 |
| inclination: | 82.5284° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 158.7286° |
| argument of perigee: | 151.6567° |
| revolutions per day: | 14.85776438 |
| mean anomaly at epoch: | 208.5786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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