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 26108.98988391 +.00000000 +00000-0 +15545-3 0 00006
2 37224 71.9704 214.4010 0014781 187.0557 173.0408 14.93501969 04
| Epoch (UTC): | 18 April 2026 23:45:25 |
| Eccentricity: | 0.0014781 |
| inclination: | 71.9704° |
| perigee height: | 577 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 214.4010° |
| argument of perigee: | 187.0557° |
| revolutions per day: | 14.93501969 |
| mean anomaly at epoch: | 173.0408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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