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 26067.58779553 +.00000000 +00000-0 +13782-3 0 00007
2 07210 81.2391 166.7909 0079497 314.8785 44.5949 14.13623642 03
| Epoch (UTC): | 08 March 2026 14:06:25 |
| Eccentricity: | 0.0079497 |
| inclination: | 81.2391° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 166.7909° |
| argument of perigee: | 314.8785° |
| revolutions per day: | 14.13623642 |
| mean anomaly at epoch: | 44.5949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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