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 68056U 26145.12936022 +.00000000 +00000-0 +39114-3 0 00002
2 68056 53.1593 53.2497 0001161 84.3093 275.8042 15.34400284 08
| Epoch (UTC): | 25 May 2026 03:06:16 |
| Eccentricity: | 0.0001161 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 53.2497° |
| argument of perigee: | 84.3093° |
| revolutions per day: | 15.34400284 |
| mean anomaly at epoch: | 275.8042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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