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 00162U 26038.97020395 +.00000000 +00000-0 +78849-4 0 00006
2 00162 47.8974 236.6740 0043597 148.3681 211.9845 14.45333866 00
| Epoch (UTC): | 07 February 2026 23:17:05 |
| Eccentricity: | 0.0043597 |
| inclination: | 47.8974° |
| perigee height: | 710 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 236.6740° |
| argument of perigee: | 148.3681° |
| revolutions per day: | 14.45333866 |
| mean anomaly at epoch: | 211.9845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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