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 60389U 26145.55380652 +.00000000 +00000-0 +33081-4 0 00000
2 60389 88.9655 282.1709 0016276 86.9858 273.3156 13.51006045 06
| Epoch (UTC): | 25 May 2026 13:17:28 |
| Eccentricity: | 0.0016276 |
| inclination: | 88.9655° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 282.1709° |
| argument of perigee: | 86.9858° |
| revolutions per day: | 13.51006045 |
| mean anomaly at epoch: | 273.3156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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