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 67005U 26145.38547319 +.00000000 +00000-0 +15942-3 0 00003
2 67005 70.0007 261.1778 0003301 269.4710 90.6071 14.98333455 00
| Epoch (UTC): | 25 May 2026 09:15:04 |
| Eccentricity: | 0.0003301 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.1778° |
| argument of perigee: | 269.4710° |
| revolutions per day: | 14.98333455 |
| mean anomaly at epoch: | 90.6071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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