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 26070.85334728 +.00000000 +00000-0 +55356-4 0 00008
2 21153 82.9300 349.4595 0027780 237.7909 184.2888 13.76344367 09
| Epoch (UTC): | 11 March 2026 20:28:49 |
| Eccentricity: | 0.0027780 |
| inclination: | 82.9300° |
| perigee height: | 956 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 349.4595° |
| argument of perigee: | 237.7909° |
| revolutions per day: | 13.76344367 |
| mean anomaly at epoch: | 184.2888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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