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 67808U 26145.10762703 +.00000000 +00000-0 +56622-3 0 00000
2 67808 97.2853 333.2287 0001549 91.4925 268.6495 15.33452480 07
| Epoch (UTC): | 25 May 2026 02:34:58 |
| Eccentricity: | 0.0001549 |
| inclination: | 97.2853° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.2287° |
| argument of perigee: | 91.4925° |
| revolutions per day: | 15.33452480 |
| mean anomaly at epoch: | 268.6495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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