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 21803U 26150.52975600 +.00000000 +00000-0 +00000-0 0 00005
2 21803 14.7896 1.7740 0001115 329.5667 16.2647 0.99295935 03
| Epoch (UTC): | 30 May 2026 12:42:50 |
| Eccentricity: | 0.0001115 |
| inclination: | 14.7896° |
| perigee height: | 36058 km |
| apogee height: | 36067 km |
| right ascension of ascending node: | 1.7740° |
| argument of perigee: | 329.5667° |
| revolutions per day: | 0.99295935 |
| mean anomaly at epoch: | 16.2647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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