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 60125U 26145.33765740 +.00000000 +00000-0 -40594-3 0 00006
2 60125 53.1595 203.2714 0000681 208.9092 151.1888 15.69971900 07
| Epoch (UTC): | 25 May 2026 08:06:13 |
| Eccentricity: | 0.0000681 |
| inclination: | 53.1595° |
| perigee height: | 359 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 203.2714° |
| argument of perigee: | 208.9092° |
| revolutions per day: | 15.69971900 |
| mean anomaly at epoch: | 151.1888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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