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 68308U 26145.30360185 +.00000000 +00000-0 +20937-2 0 00005
2 68308 97.2843 271.5233 0000733 111.0947 249.0397 15.75310479 05
| Epoch (UTC): | 25 May 2026 07:17:11 |
| Eccentricity: | 0.0000733 |
| inclination: | 97.2843° |
| perigee height: | 343 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 271.5233° |
| argument of perigee: | 111.0947° |
| revolutions per day: | 15.75310479 |
| mean anomaly at epoch: | 249.0397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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