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 60729U 26145.13075633 +.00000000 +00000-0 +82596-5 0 00008
2 60729 53.1586 99.2218 0000949 78.0583 282.0541 15.69710261 08
| Epoch (UTC): | 25 May 2026 03:08:17 |
| Eccentricity: | 0.0000949 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 99.2218° |
| argument of perigee: | 78.0583° |
| revolutions per day: | 15.69710261 |
| mean anomaly at epoch: | 282.0541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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