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 39446U 26069.86664325 +.00000000 +00000-0 +54067-3 0 00007
2 39446 97.8589 25.4028 0048372 288.0756 71.5199 14.96195831 04
| Epoch (UTC): | 10 March 2026 20:47:57 |
| Eccentricity: | 0.0048372 |
| inclination: | 97.8589° |
| perigee height: | 545 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 25.4028° |
| argument of perigee: | 288.0756° |
| revolutions per day: | 14.96195831 |
| mean anomaly at epoch: | 71.5199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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