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 41240U 26107.88612495 +.00000000 +00000-0 -32046-3 0 00002
2 41240 66.0397 252.6107 0007862 275.2308 84.7813 12.87627531 00
| Epoch (UTC): | 17 April 2026 21:16:01 |
| Eccentricity: | 0.0007862 |
| inclination: | 66.0397° |
| perigee height: | 1305 km |
| apogee height: | 1317 km |
| right ascension of ascending node: | 252.6107° |
| argument of perigee: | 275.2308° |
| revolutions per day: | 12.87627531 |
| mean anomaly at epoch: | 84.7813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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