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 68146U 26145.50827852 +.00000000 +00000-0 +74285-3 0 00002
2 68146 97.2834 167.2173 0000911 103.5748 256.5596 15.33454708 04
| Epoch (UTC): | 25 May 2026 12:11:55 |
| Eccentricity: | 0.0000911 |
| inclination: | 97.2834° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.2173° |
| argument of perigee: | 103.5748° |
| revolutions per day: | 15.33454708 |
| mean anomaly at epoch: | 256.5596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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