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 60912U 26145.34015878 +.00000000 +00000-0 +42600-4 0 00001
2 60912 53.1574 113.3700 0001224 71.7177 288.3974 15.69707458 02
| Epoch (UTC): | 25 May 2026 08:09:49 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 113.3700° |
| argument of perigee: | 71.7177° |
| revolutions per day: | 15.69707458 |
| mean anomaly at epoch: | 288.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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