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 37181U 26160.72725837 +.00000000 +00000-0 +24747-3 0 00006
2 37181 97.7843 205.5844 0073896 136.5605 224.1484 15.18332790 01
| Epoch (UTC): | 09 June 2026 17:27:15 |
| Eccentricity: | 0.0073896 |
| inclination: | 97.7843° |
| perigee height: | 460 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 205.5844° |
| argument of perigee: | 136.5605° |
| revolutions per day: | 15.18332790 |
| mean anomaly at epoch: | 224.1484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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