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 37225U 26140.35556346 +.00000000 +00000-0 +37774-4 0 00004
2 37225 71.9723 221.6141 0016753 187.3310 172.7612 14.82108542 03
| Epoch (UTC): | 20 May 2026 08:32:00 |
| Eccentricity: | 0.0016753 |
| inclination: | 71.9723° |
| perigee height: | 611 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 221.6141° |
| argument of perigee: | 187.3310° |
| revolutions per day: | 14.82108542 |
| mean anomaly at epoch: | 172.7612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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