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 68040U 26145.43820935 +.00000000 +00000-0 +64424-3 0 00006
2 68040 53.1565 51.6393 0000858 101.2409 258.8690 15.34406761 05
| Epoch (UTC): | 25 May 2026 10:31:01 |
| Eccentricity: | 0.0000858 |
| inclination: | 53.1565° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 51.6393° |
| argument of perigee: | 101.2409° |
| revolutions per day: | 15.34406761 |
| mean anomaly at epoch: | 258.8690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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