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 68272U 26145.49381964 +.00000000 +00000-0 +97944-3 0 00006
2 68272 53.1595 323.7132 0001543 102.2138 257.9037 15.34402049 01
| Epoch (UTC): | 25 May 2026 11:51:06 |
| Eccentricity: | 0.0001543 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 323.7132° |
| argument of perigee: | 102.2138° |
| revolutions per day: | 15.34402049 |
| mean anomaly at epoch: | 257.9037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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