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 60197U 26145.49639192 +.00000000 +00000-0 -34239-5 0 00004
2 60197 53.1603 325.1400 0001154 84.7426 275.3709 15.34385865 01
| Epoch (UTC): | 25 May 2026 11:54:48 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.1400° |
| argument of perigee: | 84.7426° |
| revolutions per day: | 15.34385865 |
| mean anomaly at epoch: | 275.3709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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