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 60131U 26145.38349514 +.00000000 +00000-0 +12376-4 0 00002
2 60131 53.1614 30.1227 0001130 94.7087 265.4044 15.31700268 06
| Epoch (UTC): | 25 May 2026 09:12:13 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 30.1227° |
| argument of perigee: | 94.7087° |
| revolutions per day: | 15.31700268 |
| mean anomaly at epoch: | 265.4044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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