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 60393U 26145.57853527 +.00000000 +00000-0 +12696-3 0 00001
2 60393 88.9712 282.2613 0014356 84.7013 275.5775 13.51011292 07
| Epoch (UTC): | 25 May 2026 13:53:05 |
| Eccentricity: | 0.0014356 |
| inclination: | 88.9712° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 282.2613° |
| argument of perigee: | 84.7013° |
| revolutions per day: | 13.51011292 |
| mean anomaly at epoch: | 275.5775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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