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 60062U 26145.48707889 +.00000000 +00000-0 +17007-4 0 00005
2 60062 53.1571 172.5888 0001004 67.2279 292.8845 15.69709154 00
| Epoch (UTC): | 25 May 2026 11:41:23 |
| Eccentricity: | 0.0001004 |
| inclination: | 53.1571° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 172.5888° |
| argument of perigee: | 67.2279° |
| revolutions per day: | 15.69709154 |
| mean anomaly at epoch: | 292.8845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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