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 60051U 26145.66668980 +.00000000 +00000-0 +17640-2 0 00002
2 60051 53.1600 80.6358 0001263 88.7128 118.2873 15.31670439 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 80.6358° |
| argument of perigee: | 88.7128° |
| revolutions per day: | 15.31670439 |
| mean anomaly at epoch: | 118.2873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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