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 43013U 26145.58663191 +.00000000 +00000-0 +44147-4 0 00005
2 43013 98.7766 85.2511 0001056 39.5829 320.5424 14.19506941 06
| Epoch (UTC): | 25 May 2026 14:04:44 |
| Eccentricity: | 0.0001056 |
| inclination: | 98.7766° |
| perigee height: | 826 km |
| apogee height: | 828 km |
| right ascension of ascending node: | 85.2511° |
| argument of perigee: | 39.5829° |
| revolutions per day: | 14.19506941 |
| mean anomaly at epoch: | 320.5424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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