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 39168U 26146.14375022 +.00000000 +00000-0 +00000-0 0 00003
2 39168 0.0191 296.7059 0000200 41.8781 264.3755 1.00272012 06
| Epoch (UTC): | 26 May 2026 03:27:00 |
| Eccentricity: | 0.0000200 |
| inclination: | 0.0191° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 296.7059° |
| argument of perigee: | 41.8781° |
| revolutions per day: | 1.00272012 |
| mean anomaly at epoch: | 264.3755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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