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 37673U 26152.54296014 +.00000000 +00000-0 +15217-3 0 00005
2 37673 97.9766 166.5990 0001715 110.4199 4.1278 14.78604147 01
| Epoch (UTC): | 01 June 2026 13:01:51 |
| Eccentricity: | 0.0001715 |
| inclination: | 97.9766° |
| perigee height: | 633 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 166.5990° |
| argument of perigee: | 110.4199° |
| revolutions per day: | 14.78604147 |
| mean anomaly at epoch: | 4.1278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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