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 21668U 26150.47241566 +.00000000 +00000-0 +00000-0 0 00005
2 21668 13.3958 357.1556 0003386 159.0884 34.1976 0.98794479 08
| Epoch (UTC): | 30 May 2026 11:20:16 |
| Eccentricity: | 0.0003386 |
| inclination: | 13.3958° |
| perigee height: | 36191 km |
| apogee height: | 36220 km |
| right ascension of ascending node: | 357.1556° |
| argument of perigee: | 159.0884° |
| revolutions per day: | 0.98794479 |
| mean anomaly at epoch: | 34.1976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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