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 68508U 26145.58335647 +.00000000 +00000-0 -48299-1 0 00003
2 68508 53.1595 125.3373 0001230 104.4642 168.3533 15.42254875 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001230 |
| inclination: | 53.1595° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 125.3373° |
| argument of perigee: | 104.4642° |
| revolutions per day: | 15.42254875 |
| mean anomaly at epoch: | 168.3533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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