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 68098U 26145.60572757 +.00000000 +00000-0 +31583-3 0 00004
2 68098 42.0225 351.2933 0002695 140.6700 219.4333 15.32116989 04
| Epoch (UTC): | 25 May 2026 14:32:14 |
| Eccentricity: | 0.0002695 |
| inclination: | 42.0225° |
| perigee height: | 468 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 351.2933° |
| argument of perigee: | 140.6700° |
| revolutions per day: | 15.32116989 |
| mean anomaly at epoch: | 219.4333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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