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 43445U 26140.22076066 +.00000000 +00000-0 +00000-0 0 00005
2 43445 7.0517 67.2815 0010980 168.4691 1.5319 1.02114162 01
| Epoch (UTC): | 20 May 2026 05:17:53 |
| Eccentricity: | 0.0010980 |
| inclination: | 7.0517° |
| perigee height: | 35232 km |
| apogee height: | 35324 km |
| right ascension of ascending node: | 67.2815° |
| argument of perigee: | 168.4691° |
| revolutions per day: | 1.02114162 |
| mean anomaly at epoch: | 1.5319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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