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 26072.73665332 +.00000000 +00000-0 +62048-4 0 00001
2 21153 82.9299 348.0586 0027812 232.2576 156.0387 13.76344678 03
| Epoch (UTC): | 13 March 2026 17:40:46 |
| Eccentricity: | 0.0027812 |
| inclination: | 82.9299° |
| perigee height: | 956 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 348.0586° |
| argument of perigee: | 232.2576° |
| revolutions per day: | 13.76344678 |
| mean anomaly at epoch: | 156.0387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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