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 43761U 26150.55580522 +.00000000 +00000-0 +18045-3 0 00001
2 43761 97.4183 192.0281 0012756 51.7466 308.4908 15.06475947 08
| Epoch (UTC): | 30 May 2026 13:20:21 |
| Eccentricity: | 0.0012756 |
| inclination: | 97.4183° |
| perigee height: | 538 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 192.0281° |
| argument of perigee: | 51.7466° |
| revolutions per day: | 15.06475947 |
| mean anomaly at epoch: | 308.4908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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