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 26074.98678426 +.00000000 +00000-0 +57365-4 0 00004
2 21153 82.9297 346.3847 0027913 225.7059 145.3423 13.76344927 06
| Epoch (UTC): | 15 March 2026 23:40:58 |
| Eccentricity: | 0.0027913 |
| inclination: | 82.9297° |
| perigee height: | 956 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 346.3847° |
| argument of perigee: | 225.7059° |
| revolutions per day: | 13.76344927 |
| mean anomaly at epoch: | 145.3423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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