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 26070.77286469 +.00000000 +00000-0 +80883-4 0 00008
2 07210 81.2390 163.6704 0079436 305.7166 53.6633 14.13624944 03
| Epoch (UTC): | 11 March 2026 18:32:55 |
| Eccentricity: | 0.0079436 |
| inclination: | 81.2390° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 163.6704° |
| argument of perigee: | 305.7166° |
| revolutions per day: | 14.13624944 |
| mean anomaly at epoch: | 53.6633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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