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 26072.68390650 +.00000000 +00000-0 +46415-4 0 00001
2 07210 81.2388 161.7981 0079428 300.2065 59.1258 14.13625509 07
| Epoch (UTC): | 13 March 2026 16:24:49 |
| Eccentricity: | 0.0079428 |
| inclination: | 81.2388° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 161.7981° |
| argument of perigee: | 300.2065° |
| revolutions per day: | 14.13625509 |
| mean anomaly at epoch: | 59.1258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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