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 66876U 26145.37276647 +.00000000 +00000-0 +54028-3 0 00008
2 66876 42.9972 270.3650 0000465 269.5063 90.5735 15.27599182 05
| Epoch (UTC): | 25 May 2026 08:56:47 |
| Eccentricity: | 0.0000465 |
| inclination: | 42.9972° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 270.3650° |
| argument of perigee: | 269.5063° |
| revolutions per day: | 15.27599182 |
| mean anomaly at epoch: | 90.5735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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