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 68442U 26145.62612332 +.00000000 +00000-0 +26614-3 0 00002
2 68442 97.4525 104.3565 0005741 130.5853 229.5881 15.17477296 08
| Epoch (UTC): | 25 May 2026 15:01:37 |
| Eccentricity: | 0.0005741 |
| inclination: | 97.4525° |
| perigee height: | 510 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 104.3565° |
| argument of perigee: | 130.5853° |
| revolutions per day: | 15.17477296 |
| mean anomaly at epoch: | 229.5881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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