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 60405U 26145.50058243 +.00000000 +00000-0 -28150-5 0 00005
2 60405 53.1600 67.8493 0001151 75.7120 284.4026 15.69721627 01
| Epoch (UTC): | 25 May 2026 12:00:50 |
| Eccentricity: | 0.0001151 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 67.8493° |
| argument of perigee: | 75.7120° |
| revolutions per day: | 15.69721627 |
| mean anomaly at epoch: | 284.4026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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