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 61726U 26145.61685669 +.00000000 +00000-0 +26626-4 0 00006
2 61726 53.1610 104.0786 0001365 84.4876 275.6280 15.30193258 05
| Epoch (UTC): | 25 May 2026 14:48:16 |
| Eccentricity: | 0.0001365 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 104.0786° |
| argument of perigee: | 84.4876° |
| revolutions per day: | 15.30193258 |
| mean anomaly at epoch: | 275.6280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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