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 68052U 26145.47024179 +.00000000 +00000-0 +57575-3 0 00008
2 68052 53.1604 53.2466 0000997 109.1531 250.9580 15.34402180 00
| Epoch (UTC): | 25 May 2026 11:17:08 |
| Eccentricity: | 0.0000997 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 53.2466° |
| argument of perigee: | 109.1531° |
| revolutions per day: | 15.34402180 |
| mean anomaly at epoch: | 250.9580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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