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 60928U 26145.48464206 +.00000000 +00000-0 +18375-4 0 00008
2 60928 53.1608 322.7010 0000842 69.4915 290.6194 15.69710440 01
| Epoch (UTC): | 25 May 2026 11:37:53 |
| Eccentricity: | 0.0000842 |
| inclination: | 53.1608° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 322.7010° |
| argument of perigee: | 69.4915° |
| revolutions per day: | 15.69710440 |
| mean anomaly at epoch: | 290.6194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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