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 60388U 26145.59100691 +.00000000 +00000-0 +13512-3 0 00002
2 60388 88.9730 281.7027 0016307 66.9197 293.3672 13.51011874 07
| Epoch (UTC): | 25 May 2026 14:11:02 |
| Eccentricity: | 0.0016307 |
| inclination: | 88.9730° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 281.7027° |
| argument of perigee: | 66.9197° |
| revolutions per day: | 13.51011874 |
| mean anomaly at epoch: | 293.3672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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