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 43446U 26139.02200397 +.00000000 +00000-0 +00000-0 0 00008
2 43446 7.0457 67.2669 0010823 166.5790 357.7257 1.02118587 09
| Epoch (UTC): | 19 May 2026 00:31:41 |
| Eccentricity: | 0.0010823 |
| inclination: | 7.0457° |
| perigee height: | 35232 km |
| apogee height: | 35322 km |
| right ascension of ascending node: | 67.2669° |
| argument of perigee: | 166.5790° |
| revolutions per day: | 1.02118587 |
| mean anomaly at epoch: | 357.7257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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