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 60509U 26145.49306985 +.00000000 +00000-0 +38327-3 0 00001
2 60509 97.3807 231.0386 0003017 50.2000 309.9513 15.43287559 06
| Epoch (UTC): | 25 May 2026 11:50:01 |
| Eccentricity: | 0.0003017 |
| inclination: | 97.3807° |
| perigee height: | 434 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 231.0386° |
| argument of perigee: | 50.2000° |
| revolutions per day: | 15.43287559 |
| mean anomaly at epoch: | 309.9513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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