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 00011U 26037.76377065 +.00000000 +00000-0 +38099-3 0 00006
2 00011 32.8629 218.6794 1446533 34.7260 333.9724 11.90221209 07
| Epoch (UTC): | 06 February 2026 18:19:49 |
| Eccentricity: | 0.1446533 |
| inclination: | 32.8629° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 218.6794° |
| argument of perigee: | 34.7260° |
| revolutions per day: | 11.90221209 |
| mean anomaly at epoch: | 333.9724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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