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 60419U 26145.45804853 +.00000000 +00000-0 +38557-3 0 00009
2 60419 53.0030 156.7798 0001344 87.0500 273.0633 14.87671799 01
| Epoch (UTC): | 25 May 2026 10:59:35 |
| Eccentricity: | 0.0001344 |
| inclination: | 53.0030° |
| perigee height: | 604 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 156.7798° |
| argument of perigee: | 87.0500° |
| revolutions per day: | 14.87671799 |
| mean anomaly at epoch: | 273.0633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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