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 68186U 26145.36915376 +.00000000 +00000-0 +77853-3 0 00003
2 68186 53.1564 269.8473 0002053 80.9633 279.1602 15.35439280 00
| Epoch (UTC): | 25 May 2026 08:51:34 |
| Eccentricity: | 0.0002053 |
| inclination: | 53.1564° |
| perigee height: | 458 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 269.8473° |
| argument of perigee: | 80.9633° |
| revolutions per day: | 15.35439280 |
| mean anomaly at epoch: | 279.1602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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