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 67025U 26145.42734066 +.00000000 +00000-0 +29942-3 0 00002
2 67025 70.0007 260.9172 0003191 272.0937 87.9857 14.98348041 03
| Epoch (UTC): | 25 May 2026 10:15:22 |
| Eccentricity: | 0.0003191 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.9172° |
| argument of perigee: | 272.0937° |
| revolutions per day: | 14.98348041 |
| mean anomaly at epoch: | 87.9857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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