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 68678U 26145.57747801 +.00000000 +00000-0 +32429-3 0 00008
2 68678 97.2856 17.1828 0001836 98.4649 261.6802 15.33436580 02
| Epoch (UTC): | 25 May 2026 13:51:34 |
| Eccentricity: | 0.0001836 |
| inclination: | 97.2856° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.1828° |
| argument of perigee: | 98.4649° |
| revolutions per day: | 15.33436580 |
| mean anomaly at epoch: | 261.6802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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