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 68679U 26145.11796118 +.00000000 +00000-0 +57933-3 0 00001
2 68679 97.2850 16.7358 0001466 92.9670 267.1741 15.33462983 01
| Epoch (UTC): | 25 May 2026 02:49:51 |
| Eccentricity: | 0.0001466 |
| inclination: | 97.2850° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 16.7358° |
| argument of perigee: | 92.9670° |
| revolutions per day: | 15.33462983 |
| mean anomaly at epoch: | 267.1741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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