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 67588U 26144.76495304 +.00000000 +00000-0 +00000-0 0 00002
2 67588 55.0742 89.6948 0022702 256.4817 103.2392 2.00571625 07
| Epoch (UTC): | 24 May 2026 18:21:31 |
| Eccentricity: | 0.0022702 |
| inclination: | 55.0742° |
| perigee height: | 20121 km |
| apogee height: | 20242 km |
| right ascension of ascending node: | 89.6948° |
| argument of perigee: | 256.4817° |
| revolutions per day: | 2.00571625 |
| mean anomaly at epoch: | 103.2392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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