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 21056U 26150.27336389 +.00000000 +00000-0 +00000-0 0 00002
2 21056 14.8893 1.7559 0002403 164.3796 20.4783 0.98942454 00
| Epoch (UTC): | 30 May 2026 06:33:38 |
| Eccentricity: | 0.0002403 |
| inclination: | 14.8893° |
| perigee height: | 36153 km |
| apogee height: | 36174 km |
| right ascension of ascending node: | 1.7559° |
| argument of perigee: | 164.3796° |
| revolutions per day: | 0.98942454 |
| mean anomaly at epoch: | 20.4783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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