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 60738U 26145.08061773 +.00000000 +00000-0 +74365-6 0 00008
2 60738 53.1604 273.8122 0000747 87.9023 272.2064 15.30195117 03
| Epoch (UTC): | 25 May 2026 01:56:05 |
| Eccentricity: | 0.0000747 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 273.8122° |
| argument of perigee: | 87.9023° |
| revolutions per day: | 15.30195117 |
| mean anomaly at epoch: | 272.2064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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