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 60089U 26145.62353397 +.00000000 +00000-0 +13424-3 0 00009
2 60089 28.9959 260.0948 0005125 165.0153 195.0593 14.83484300 07
| Epoch (UTC): | 25 May 2026 14:57:53 |
| Eccentricity: | 0.0005125 |
| inclination: | 28.9959° |
| perigee height: | 615 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 260.0948° |
| argument of perigee: | 165.0153° |
| revolutions per day: | 14.83484300 |
| mean anomaly at epoch: | 195.0593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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