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 07210U 26065.53519471 +.00000000 +00000-0 +13126-3 0 00003
2 07210 81.2390 168.8017 0079577 320.7482 38.7936 14.13622671 06
| Epoch (UTC): | 06 March 2026 12:50:40 |
| Eccentricity: | 0.0079577 |
| inclination: | 81.2390° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 168.8017° |
| argument of perigee: | 320.7482° |
| revolutions per day: | 14.13622671 |
| mean anomaly at epoch: | 38.7936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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