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 60048U 26145.01564595 +.00000000 +00000-0 +17680-4 0 00000
2 60048 53.1589 249.6764 0000974 62.2102 297.9014 15.69710089 00
| Epoch (UTC): | 25 May 2026 00:22:31 |
| Eccentricity: | 0.0000974 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 249.6764° |
| argument of perigee: | 62.2102° |
| revolutions per day: | 15.69710089 |
| mean anomaly at epoch: | 297.9014° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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