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 55777U 26145.11366491 +.00000000 +00000-0 +15227-4 0 00004
2 55777 70.0000 31.6484 0002633 271.2646 88.8212 14.98333719 05
| Epoch (UTC): | 25 May 2026 02:43:40 |
| Eccentricity: | 0.0002633 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.6484° |
| argument of perigee: | 271.2646° |
| revolutions per day: | 14.98333719 |
| mean anomaly at epoch: | 88.8212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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