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 21153U 26074.51061007 +.00000000 +00000-0 +54851-4 0 00001
2 21153 82.9298 346.7389 0027881 227.0834 305.9280 13.76344849 00
| Epoch (UTC): | 15 March 2026 12:15:16 |
| Eccentricity: | 0.0027881 |
| inclination: | 82.9298° |
| perigee height: | 956 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 346.7389° |
| argument of perigee: | 227.0834° |
| revolutions per day: | 13.76344849 |
| mean anomaly at epoch: | 305.9280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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