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 13777U 26150.51384616 +.00000000 +00000-0 +16893-3 0 00006
2 13777 99.0537 332.3131 0018737 19.2829 340.9041 14.00911382 03
| Epoch (UTC): | 30 May 2026 12:19:56 |
| Eccentricity: | 0.0018737 |
| inclination: | 99.0537° |
| perigee height: | 877 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 332.3131° |
| argument of perigee: | 19.2829° |
| revolutions per day: | 14.00911382 |
| mean anomaly at epoch: | 340.9041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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