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 68064U 26145.58335647 +.00000000 +00000-0 +17566-2 0 00003
2 68064 53.1605 50.6191 0001181 86.7278 158.4049 15.34356092 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 50.6191° |
| argument of perigee: | 86.7278° |
| revolutions per day: | 15.34356092 |
| mean anomaly at epoch: | 158.4049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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