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 61711U 26145.32605204 +.00000000 +00000-0 +26710-4 0 00009
2 61711 53.1604 105.1080 0001248 92.7837 267.3307 15.30187103 00
| Epoch (UTC): | 25 May 2026 07:49:30 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.1080° |
| argument of perigee: | 92.7837° |
| revolutions per day: | 15.30187103 |
| mean anomaly at epoch: | 267.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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