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 43677U 26106.46723905 +.00000000 +00000-0 +14432-3 0 00008
2 43677 98.0792 296.2351 0008916 329.2109 30.8591 15.02676412 02
| Epoch (UTC): | 16 April 2026 11:12:49 |
| Eccentricity: | 0.0008916 |
| inclination: | 98.0792° |
| perigee height: | 552 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 296.2351° |
| argument of perigee: | 329.2109° |
| revolutions per day: | 15.02676412 |
| mean anomaly at epoch: | 30.8591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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