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 67037U 26144.91217205 +.00000000 +00000-0 +10687-2 0 00004
2 67037 43.0039 327.8578 0001812 269.6241 90.4403 15.27598752 07
| Epoch (UTC): | 24 May 2026 21:53:31 |
| Eccentricity: | 0.0001812 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.8578° |
| argument of perigee: | 269.6241° |
| revolutions per day: | 15.27598752 |
| mean anomaly at epoch: | 90.4403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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