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 40043U 26072.36397095 +.00000000 +00000-0 +31429-3 0 00005
2 40043 97.7677 224.6702 0050134 30.4793 329.9319 14.84748887 03
| Epoch (UTC): | 13 March 2026 08:44:07 |
| Eccentricity: | 0.0050134 |
| inclination: | 97.7677° |
| perigee height: | 579 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 224.6702° |
| argument of perigee: | 30.4793° |
| revolutions per day: | 14.84748887 |
| mean anomaly at epoch: | 329.9319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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