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 68681U 26145.43880334 +.00000000 +00000-0 +76905-3 0 00003
2 68681 97.2859 17.0637 0002047 87.1333 273.0144 15.33450605 06
| Epoch (UTC): | 25 May 2026 10:31:52 |
| Eccentricity: | 0.0002047 |
| inclination: | 97.2859° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.0637° |
| argument of perigee: | 87.1333° |
| revolutions per day: | 15.33450605 |
| mean anomaly at epoch: | 273.0144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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