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 02674U 26053.81167153 +.00000000 +00000-0 +96003-3 0 00001
2 02674 39.9154 209.5203 0207862 181.8561 178.1466 14.73422936 02
| Epoch (UTC): | 22 February 2026 19:28:48 |
| Eccentricity: | 0.0207862 |
| inclination: | 39.9154° |
| perigee height: | 504 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 209.5203° |
| argument of perigee: | 181.8561° |
| revolutions per day: | 14.73422936 |
| mean anomaly at epoch: | 178.1466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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