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 60195U 26145.27894054 +.00000000 +00000-0 +47170-5 0 00005
2 60195 53.1576 143.6646 0000846 75.3908 284.7203 15.69698500 05
| Epoch (UTC): | 25 May 2026 06:41:40 |
| Eccentricity: | 0.0000846 |
| inclination: | 53.1576° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 143.6646° |
| argument of perigee: | 75.3908° |
| revolutions per day: | 15.69698500 |
| mean anomaly at epoch: | 284.7203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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