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 22220U 26074.27524730 +.00000000 +00000-0 +32085-4 0 00002
2 22220 71.0006 176.6087 0010530 86.0336 341.6978 14.16859222 02
| Epoch (UTC): | 15 March 2026 06:36:21 |
| Eccentricity: | 0.0010530 |
| inclination: | 71.0006° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 176.6087° |
| argument of perigee: | 86.0336° |
| revolutions per day: | 14.16859222 |
| mean anomaly at epoch: | 341.6978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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