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 60401U 26145.20176273 +.00000000 +00000-0 +11359-4 0 00003
2 60401 53.1591 68.8168 0000940 95.6041 264.5084 15.69714223 01
| Epoch (UTC): | 25 May 2026 04:50:32 |
| Eccentricity: | 0.0000940 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 68.8168° |
| argument of perigee: | 95.6041° |
| revolutions per day: | 15.69714223 |
| mean anomaly at epoch: | 264.5084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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