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 60728U 26145.13566301 +.00000000 +00000-0 +27005-4 0 00007
2 60728 53.1592 99.2672 0001095 68.3961 291.7173 15.69702784 02
| Epoch (UTC): | 25 May 2026 03:15:21 |
| Eccentricity: | 0.0001095 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 99.2672° |
| argument of perigee: | 68.3961° |
| revolutions per day: | 15.69702784 |
| mean anomaly at epoch: | 291.7173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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