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 38771U 26106.87860771 +.00000000 +00000-0 +51331-4 0 00005
2 38771 98.6564 159.5841 0003056 143.4586 216.6800 14.21430736 08
| Epoch (UTC): | 16 April 2026 21:05:11 |
| Eccentricity: | 0.0003056 |
| inclination: | 98.6564° |
| perigee height: | 818 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 159.5841° |
| argument of perigee: | 143.4586° |
| revolutions per day: | 14.21430736 |
| mean anomaly at epoch: | 216.6800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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