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 61713U 26145.18498076 +.00000000 +00000-0 +48085-5 0 00002
2 61713 53.1598 106.3639 0001155 84.1411 275.9722 15.30194060 03
| Epoch (UTC): | 25 May 2026 04:26:22 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.3639° |
| argument of perigee: | 84.1411° |
| revolutions per day: | 15.30194060 |
| mean anomaly at epoch: | 275.9722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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