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 26067.87298103 +.00000000 +00000-0 +89114-4 0 00001
2 21153 82.9300 351.6765 0027707 246.5144 176.6611 13.76344059 08
| Epoch (UTC): | 08 March 2026 20:57:05 |
| Eccentricity: | 0.0027707 |
| inclination: | 82.9300° |
| perigee height: | 957 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 351.6765° |
| argument of perigee: | 246.5144° |
| revolutions per day: | 13.76344059 |
| mean anomaly at epoch: | 176.6611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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