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 60313U 26145.36836419 +.00000000 +00000-0 -11521-4 0 00009
2 60313 53.1588 128.4917 0000694 89.4459 270.6639 15.69690730 04
| Epoch (UTC): | 25 May 2026 08:50:26 |
| Eccentricity: | 0.0000694 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 128.4917° |
| argument of perigee: | 89.4459° |
| revolutions per day: | 15.69690730 |
| mean anomaly at epoch: | 270.6639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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