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 67004U 26145.56905556 +.00000000 +00000-0 +22140-3 0 00001
2 67004 70.0007 260.6132 0003090 269.1161 90.9644 14.98336067 00
| Epoch (UTC): | 25 May 2026 13:39:26 |
| Eccentricity: | 0.0003090 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 260.6132° |
| argument of perigee: | 269.1161° |
| revolutions per day: | 14.98336067 |
| mean anomaly at epoch: | 90.9644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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