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 67878U 26145.43387344 +.00000000 +00000-0 +68437-3 0 00004
2 67878 53.1593 207.9067 0000859 52.3217 307.7862 15.30202077 07
| Epoch (UTC): | 25 May 2026 10:24:46 |
| Eccentricity: | 0.0000859 |
| inclination: | 53.1593° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9067° |
| argument of perigee: | 52.3217° |
| revolutions per day: | 15.30202077 |
| mean anomaly at epoch: | 307.7862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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