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 60930U 26145.47483108 +.00000000 +00000-0 +23293-4 0 00007
2 60930 53.1582 322.6333 0000802 104.5404 255.5703 15.69701249 05
| Epoch (UTC): | 25 May 2026 11:23:45 |
| Eccentricity: | 0.0000802 |
| inclination: | 53.1582° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.6333° |
| argument of perigee: | 104.5404° |
| revolutions per day: | 15.69701249 |
| mean anomaly at epoch: | 255.5703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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