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 68904U 26145.28260970 +.00000000 +00000-0 +11260-2 0 00004
2 68904 97.2871 341.0911 0002407 82.4824 277.6701 15.49202601 03
| Epoch (UTC): | 25 May 2026 06:46:57 |
| Eccentricity: | 0.0002407 |
| inclination: | 97.2871° |
| perigee height: | 417 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 341.0911° |
| argument of perigee: | 82.4824° |
| revolutions per day: | 15.49202601 |
| mean anomaly at epoch: | 277.6701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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