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 68157U 26145.51643367 +.00000000 +00000-0 +87109-3 0 00001
2 68157 97.2846 167.2056 0000358 194.0430 166.0803 15.33459520 00
| Epoch (UTC): | 25 May 2026 12:23:39 |
| Eccentricity: | 0.0000358 |
| inclination: | 97.2846° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.2056° |
| argument of perigee: | 194.0430° |
| revolutions per day: | 15.33459520 |
| mean anomaly at epoch: | 166.0803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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