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 67527U 26145.49659911 +.00000000 +00000-0 +73012-4 0 00009
2 67527 50.0091 76.9867 0000923 26.8092 333.2828 13.29327992 04
| Epoch (UTC): | 25 May 2026 11:55:06 |
| Eccentricity: | 0.0000923 |
| inclination: | 50.0091° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 76.9867° |
| argument of perigee: | 26.8092° |
| revolutions per day: | 13.29327992 |
| mean anomaly at epoch: | 333.2828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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