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 26159.84453122 +.00000000 +00000-0 +92086-4 0 00006
2 21153 82.9251 283.2107 0028668 352.9554 120.7600 13.76365450 03
| Epoch (UTC): | 08 June 2026 20:16:07 |
| Eccentricity: | 0.0028668 |
| inclination: | 82.9251° |
| perigee height: | 956 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 283.2107° |
| argument of perigee: | 352.9554° |
| revolutions per day: | 13.76365450 |
| mean anomaly at epoch: | 120.7600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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