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 41948U 26109.07935644 +.00000000 +00000-0 +12878-5 0 00006
2 41948 97.4161 169.4716 0005747 91.4602 268.7291 15.19213585 00
| Epoch (UTC): | 19 April 2026 01:54:16 |
| Eccentricity: | 0.0005747 |
| inclination: | 97.4161° |
| perigee height: | 504 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 169.4716° |
| argument of perigee: | 91.4602° |
| revolutions per day: | 15.19213585 |
| mean anomaly at epoch: | 268.7291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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