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 41194U 26145.31950984 +.00000000 +00000-0 +00000-0 0 00009
2 41194 0.3709 83.2050 0002440 130.5394 249.8364 1.00266999 01
| Epoch (UTC): | 25 May 2026 07:40:05 |
| Eccentricity: | 0.0002440 |
| inclination: | 0.3709° |
| perigee height: | 35778 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 83.2050° |
| argument of perigee: | 130.5394° |
| revolutions per day: | 1.00266999 |
| mean anomaly at epoch: | 249.8364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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