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 60934U 26145.51887998 +.00000000 +00000-0 +43097-4 0 00005
2 60934 53.1568 322.1870 0001139 72.3077 287.8065 15.69716174 08
| Epoch (UTC): | 25 May 2026 12:27:11 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.1568° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.1870° |
| argument of perigee: | 72.3077° |
| revolutions per day: | 15.69716174 |
| mean anomaly at epoch: | 287.8065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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