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 45278U 26088.00285367 +.00000000 +00000-0 +50916-2 0 00007
2 45278 82.5662 72.0626 0143118 150.9543 209.9675 13.80445425 09
| Epoch (UTC): | 29 March 2026 00:04:06 |
| Eccentricity: | 0.0143118 |
| inclination: | 82.5662° |
| perigee height: | 857 km |
| apogee height: | 1067 km |
| right ascension of ascending node: | 72.0626° |
| argument of perigee: | 150.9543° |
| revolutions per day: | 13.80445425 |
| mean anomaly at epoch: | 209.9675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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