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 41021U 26144.81997093 +.00000000 +00000-0 +00000-0 0 00004
2 41021 0.2148 91.0070 0007559 100.9464 89.0445 1.00267451 08
| Epoch (UTC): | 24 May 2026 19:40:45 |
| Eccentricity: | 0.0007559 |
| inclination: | 0.2148° |
| perigee height: | 35756 km |
| apogee height: | 35820 km |
| right ascension of ascending node: | 91.0070° |
| argument of perigee: | 100.9464° |
| revolutions per day: | 1.00267451 |
| mean anomaly at epoch: | 89.0445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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