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 68273U 26145.48926971 +.00000000 +00000-0 +70356-3 0 00007
2 68273 53.1596 321.5237 0001245 113.4012 246.7123 15.35426758 05
| Epoch (UTC): | 25 May 2026 11:44:32 |
| Eccentricity: | 0.0001245 |
| inclination: | 53.1596° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 321.5237° |
| argument of perigee: | 113.4012° |
| revolutions per day: | 15.35426758 |
| mean anomaly at epoch: | 246.7123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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