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 68288U 26145.50585816 +.00000000 +00000-0 +72980-3 0 00000
2 68288 53.1588 321.6305 0000531 323.8710 36.2256 15.34412110 03
| Epoch (UTC): | 25 May 2026 12:08:26 |
| Eccentricity: | 0.0000531 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 321.6305° |
| argument of perigee: | 323.8710° |
| revolutions per day: | 15.34412110 |
| mean anomaly at epoch: | 36.2256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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