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 68176U 26144.74539360 +.00000000 +00000-0 +61613-3 0 00005
2 68176 53.1609 273.0479 0001047 79.3784 280.7337 15.34399837 08
| Epoch (UTC): | 24 May 2026 17:53:22 |
| Eccentricity: | 0.0001047 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 273.0479° |
| argument of perigee: | 79.3784° |
| revolutions per day: | 15.34399837 |
| mean anomaly at epoch: | 280.7337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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