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 26073.61172463 +.00000000 +00000-0 +60832-3 0 00009
2 39446 97.8593 29.1621 0047907 275.1721 84.4033 14.96242909 00
| Epoch (UTC): | 14 March 2026 14:40:53 |
| Eccentricity: | 0.0047907 |
| inclination: | 97.8593° |
| perigee height: | 545 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 29.1621° |
| argument of perigee: | 275.1721° |
| revolutions per day: | 14.96242909 |
| mean anomaly at epoch: | 84.4033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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