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 68091U 26145.40182124 +.00000000 +00000-0 +37063-3 0 00009
2 68091 53.1581 181.4388 0001265 72.6102 287.5039 15.34403079 04
| Epoch (UTC): | 25 May 2026 09:38:37 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.4388° |
| argument of perigee: | 72.6102° |
| revolutions per day: | 15.34403079 |
| mean anomaly at epoch: | 287.5039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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