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 68438U 26144.86001650 +.00000000 +00000-0 +48403-3 0 00007
2 68438 97.4509 103.6850 0005455 109.3427 250.8398 15.19031909 06
| Epoch (UTC): | 24 May 2026 20:38:25 |
| Eccentricity: | 0.0005455 |
| inclination: | 97.4509° |
| perigee height: | 505 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 103.6850° |
| argument of perigee: | 109.3427° |
| revolutions per day: | 15.19031909 |
| mean anomaly at epoch: | 250.8398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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