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 43812U 26150.56427751 +.00000000 +00000-0 +26490-3 0 00006
2 43812 97.3569 187.8112 0005139 197.3227 162.7827 15.08558325 01
| Epoch (UTC): | 30 May 2026 13:32:33 |
| Eccentricity: | 0.0005139 |
| inclination: | 97.3569° |
| perigee height: | 537 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 187.8112° |
| argument of perigee: | 197.3227° |
| revolutions per day: | 15.08558325 |
| mean anomaly at epoch: | 162.7827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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