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 37779U 26064.19558706 +.00000000 +00000-0 +00000-0 0 00005
2 37779 0.4193 85.7587 0002621 306.5863 239.0487 1.00278945 03
| Epoch (UTC): | 05 March 2026 04:41:38 |
| Eccentricity: | 0.0002621 |
| inclination: | 0.4193° |
| perigee height: | 35774 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 85.7587° |
| argument of perigee: | 306.5863° |
| revolutions per day: | 1.00278945 |
| mean anomaly at epoch: | 239.0487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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