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 26074.81547750 +.00000000 +00000-0 +43342-3 0 00004
2 39446 97.8599 30.3705 0047780 271.0316 88.5430 14.96254353 09
| Epoch (UTC): | 15 March 2026 19:34:17 |
| Eccentricity: | 0.0047780 |
| inclination: | 97.8599° |
| perigee height: | 545 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 30.3705° |
| argument of perigee: | 271.0316° |
| revolutions per day: | 14.96254353 |
| mean anomaly at epoch: | 88.5430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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