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 41032U 26141.56155514 +.00000000 +00000-0 +00000-0 0 00009
2 41032 63.4971 349.8445 7205430 274.6485 13.7166 2.00973371 02
| Epoch (UTC): | 21 May 2026 13:28:38 |
| Eccentricity: | 0.7205430 |
| inclination: | 63.4971° |
| perigee height: | 1034 km |
| apogee height: | 39258 km |
| right ascension of ascending node: | 349.8445° |
| argument of perigee: | 274.6485° |
| revolutions per day: | 2.00973371 |
| mean anomaly at epoch: | 13.7166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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