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,
| Epoch (UTC): | 13 January 2026 12:02:43 |
| Eccentricity: | 0.0010676 |
| inclination: | 98.8954° |
| perigee height: | 771 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 30.9658° |
| argument of perigee: | 302.6414° |
| revolutions per day: | 14.34060385 |
| mean anomaly at epoch: | 57.3739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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