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 37224U 26145.35867941 +.00000000 +00000-0 +18073-3 0 00004
2 37224 71.9680 132.0447 0012521 113.2479 247.0011 14.93628546 03
| Epoch (UTC): | 25 May 2026 08:36:29 |
| Eccentricity: | 0.0012521 |
| inclination: | 71.9680° |
| perigee height: | 578 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 132.0447° |
| argument of perigee: | 113.2479° |
| revolutions per day: | 14.93628546 |
| mean anomaly at epoch: | 247.0011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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