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 68137U 26145.38313778 +.00000000 +00000-0 +78358-4 0 00001
2 68137 50.0044 137.6165 0000176 10.4720 349.6156 13.29330662 06
| Epoch (UTC): | 25 May 2026 09:11:43 |
| Eccentricity: | 0.0000176 |
| inclination: | 50.0044° |
| perigee height: | 1149 km |
| apogee height: | 1149 km |
| right ascension of ascending node: | 137.6165° |
| argument of perigee: | 10.4720° |
| revolutions per day: | 13.29330662 |
| mean anomaly at epoch: | 349.6156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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