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 68946U 26145.49717825 +.00000000 +00000-0 +83653-3 0 00005
2 68946 51.8744 176.9375 0003721 54.1438 305.9893 15.35572557 02
| Epoch (UTC): | 25 May 2026 11:55:56 |
| Eccentricity: | 0.0003721 |
| inclination: | 51.8744° |
| perigee height: | 457 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 176.9375° |
| argument of perigee: | 54.1438° |
| revolutions per day: | 15.35572557 |
| mean anomaly at epoch: | 305.9893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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