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 62711U 26145.13418036 +.00000000 +00000-0 +51886-3 0 00005
2 62711 97.7230 227.8571 0003532 193.2294 166.8839 15.03348739 06
| Epoch (UTC): | 25 May 2026 03:13:13 |
| Eccentricity: | 0.0003532 |
| inclination: | 97.7230° |
| perigee height: | 554 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 227.8571° |
| argument of perigee: | 193.2294° |
| revolutions per day: | 15.03348739 |
| mean anomaly at epoch: | 166.8839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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