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 26069.20031681 +.00000000 +00000-0 +78836-4 0 00005
2 21153 82.9300 350.6890 0027741 242.6459 273.5540 13.76344225 03
| Epoch (UTC): | 10 March 2026 04:48:27 |
| Eccentricity: | 0.0027741 |
| inclination: | 82.9300° |
| perigee height: | 956 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 350.6890° |
| argument of perigee: | 242.6459° |
| revolutions per day: | 13.76344225 |
| mean anomaly at epoch: | 273.5540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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