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 41783U 26106.24958069 +.00000000 +00000-0 +85547-4 0 00007
2 41783 97.8327 105.8344 0032554 57.5075 302.9270 14.67108039 06
| Epoch (UTC): | 16 April 2026 05:59:23 |
| Eccentricity: | 0.0032554 |
| inclination: | 97.8327° |
| perigee height: | 647 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 105.8344° |
| argument of perigee: | 57.5075° |
| revolutions per day: | 14.67108039 |
| mean anomaly at epoch: | 302.9270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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