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 37227U 26159.40264478 +.00000000 +00000-0 +11215-3 0 00005
2 37227 71.9646 155.5318 0013210 136.2946 223.9269 14.85237569 05
| Epoch (UTC): | 08 June 2026 09:39:48 |
| Eccentricity: | 0.0013210 |
| inclination: | 71.9646° |
| perigee height: | 604 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 155.5318° |
| argument of perigee: | 136.2946° |
| revolutions per day: | 14.85237569 |
| mean anomaly at epoch: | 223.9269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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