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 41745U 26144.39920993 +.00000000 +00000-0 +00000-0 0 00005
2 41745 4.1119 77.5597 0011481 149.6685 281.5069 1.00277427 04
| Epoch (UTC): | 24 May 2026 09:34:51 |
| Eccentricity: | 0.0011481 |
| inclination: | 4.1119° |
| perigee height: | 35737 km |
| apogee height: | 35833 km |
| right ascension of ascending node: | 77.5597° |
| argument of perigee: | 149.6685° |
| revolutions per day: | 1.00277427 |
| mean anomaly at epoch: | 281.5069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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