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 68093U 26145.36614138 +.00000000 +00000-0 +56315-3 0 00002
2 68093 53.1596 181.9313 0001552 90.9717 269.1463 15.34405368 09
| Epoch (UTC): | 25 May 2026 08:47:14 |
| Eccentricity: | 0.0001552 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.9313° |
| argument of perigee: | 90.9717° |
| revolutions per day: | 15.34405368 |
| mean anomaly at epoch: | 269.1463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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