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 41921U 26145.27153891 +.00000000 +00000-0 +79565-4 0 00000
2 41921 86.3971 66.4490 0002412 90.0029 270.1443 14.34218191 06
| Epoch (UTC): | 25 May 2026 06:31:00 |
| Eccentricity: | 0.0002412 |
| inclination: | 86.3971° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 66.4490° |
| argument of perigee: | 90.0029° |
| revolutions per day: | 14.34218191 |
| mean anomaly at epoch: | 270.1443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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