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 67023U 26145.39398648 +.00000000 +00000-0 +34279-3 0 00007
2 67023 70.0007 261.2028 0003157 269.1343 90.9454 14.98336848 04
| Epoch (UTC): | 25 May 2026 09:27:20 |
| Eccentricity: | 0.0003157 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.2028° |
| argument of perigee: | 269.1343° |
| revolutions per day: | 14.98336848 |
| mean anomaly at epoch: | 90.9454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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