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 68081U 26145.47279669 +.00000000 +00000-0 +31250-3 0 00008
2 68081 53.1583 179.7453 0000817 81.3002 278.8093 15.34397126 04
| Epoch (UTC): | 25 May 2026 11:20:49 |
| Eccentricity: | 0.0000817 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 179.7453° |
| argument of perigee: | 81.3002° |
| revolutions per day: | 15.34397126 |
| mean anomaly at epoch: | 278.8093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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