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 67884U 26145.35504032 +.00000000 +00000-0 +64757-3 0 00008
2 67884 97.2859 78.8208 0001410 86.8900 273.2504 15.33456155 06
| Epoch (UTC): | 25 May 2026 08:31:15 |
| Eccentricity: | 0.0001410 |
| inclination: | 97.2859° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 78.8208° |
| argument of perigee: | 86.8900° |
| revolutions per day: | 15.33456155 |
| mean anomaly at epoch: | 273.2504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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