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 67015U 26145.56488076 +.00000000 +00000-0 +17757-3 0 00004
2 67015 70.0011 260.5978 0003326 270.2449 89.8329 14.98334958 02
| Epoch (UTC): | 25 May 2026 13:33:25 |
| Eccentricity: | 0.0003326 |
| inclination: | 70.0011° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.5978° |
| argument of perigee: | 270.2449° |
| revolutions per day: | 14.98334958 |
| mean anomaly at epoch: | 89.8329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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