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 68399U 26145.64298711 +.00000000 +00000-0 +55314-3 0 00005
2 68399 97.2850 288.2748 0001965 88.6452 271.5016 15.33456321 06
| Epoch (UTC): | 25 May 2026 15:25:54 |
| Eccentricity: | 0.0001965 |
| inclination: | 97.2850° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 288.2748° |
| argument of perigee: | 88.6452° |
| revolutions per day: | 15.33456321 |
| mean anomaly at epoch: | 271.5016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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