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 68377U 26144.97339609 +.00000000 +00000-0 +80795-4 0 00000
2 68377 97.4393 152.6194 0001680 81.1837 278.9588 15.19719939 00
| Epoch (UTC): | 24 May 2026 23:21:41 |
| Eccentricity: | 0.0001680 |
| inclination: | 97.4393° |
| perigee height: | 506 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 152.6194° |
| argument of perigee: | 81.1837° |
| revolutions per day: | 15.19719939 |
| mean anomaly at epoch: | 278.9588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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