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 60340U 26145.23225852 +.00000000 +00000-0 +13787-3 0 00002
2 60340 53.1602 80.1282 0001024 92.1973 267.9145 15.30199331 00
| Epoch (UTC): | 25 May 2026 05:34:27 |
| Eccentricity: | 0.0001024 |
| inclination: | 53.1602° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.1282° |
| argument of perigee: | 92.1973° |
| revolutions per day: | 15.30199331 |
| mean anomaly at epoch: | 267.9145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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