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 26153.08500355 +.00000000 +00000-0 +16489-3 0 00002
2 13777 99.0539 334.8609 0018568 12.0924 348.0683 14.00912675 08
| Epoch (UTC): | 02 June 2026 02:02:24 |
| Eccentricity: | 0.0018568 |
| inclination: | 99.0539° |
| perigee height: | 877 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 334.8609° |
| argument of perigee: | 12.0924° |
| revolutions per day: | 14.00912675 |
| mean anomaly at epoch: | 348.0683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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