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 68912U 26145.49823713 +.00000000 +00000-0 +62922-3 0 00008
2 68912 97.2859 341.2554 0001830 94.9596 265.1864 15.49221585 00
| Epoch (UTC): | 25 May 2026 11:57:27 |
| Eccentricity: | 0.0001830 |
| inclination: | 97.2859° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.2554° |
| argument of perigee: | 94.9596° |
| revolutions per day: | 15.49221585 |
| mean anomaly at epoch: | 265.1864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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