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 68080U 26145.39082469 +.00000000 +00000-0 +41373-3 0 00005
2 68080 53.1580 179.9256 0001068 69.7933 290.3184 15.34401905 06
| Epoch (UTC): | 25 May 2026 09:22:47 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 179.9256° |
| argument of perigee: | 69.7933° |
| revolutions per day: | 15.34401905 |
| mean anomaly at epoch: | 290.3184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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