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 68311U 26145.33643215 +.00000000 +00000-0 +81401-3 0 00004
2 68311 97.2854 271.6330 0002297 17.9066 342.2280 15.75206092 05
| Epoch (UTC): | 25 May 2026 08:04:27 |
| Eccentricity: | 0.0002297 |
| inclination: | 97.2854° |
| perigee height: | 343 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 271.6330° |
| argument of perigee: | 17.9066° |
| revolutions per day: | 15.75206092 |
| mean anomaly at epoch: | 342.2280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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