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 39211U 26161.53895111 +.00000000 +00000-0 +27622-3 0 00000
2 39211 97.9610 84.6488 0063210 301.0228 58.4818 15.37996049 03
| Epoch (UTC): | 10 June 2026 12:56:05 |
| Eccentricity: | 0.0063210 |
| inclination: | 97.9610° |
| perigee height: | 409 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 84.6488° |
| argument of perigee: | 301.0228° |
| revolutions per day: | 15.37996049 |
| mean anomaly at epoch: | 58.4818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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