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 04132U 26100.17813529 +.00000000 +00000-0 +56243-3 0 00001
2 04132 69.9921 65.6477 0011323 233.0669 126.9419 14.31831671 09
| Epoch (UTC): | 10 April 2026 04:16:30 |
| Eccentricity: | 0.0011323 |
| inclination: | 69.9921° |
| perigee height: | 778 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 65.6477° |
| argument of perigee: | 233.0669° |
| revolutions per day: | 14.31831671 |
| mean anomaly at epoch: | 126.9419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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