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 55760U 26145.18482486 +.00000000 +00000-0 -22716-5 0 00009
2 55760 70.0010 51.3765 0002689 268.0963 91.9888 14.98332629 09
| Epoch (UTC): | 25 May 2026 04:26:08 |
| Eccentricity: | 0.0002689 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.3765° |
| argument of perigee: | 268.0963° |
| revolutions per day: | 14.98332629 |
| mean anomaly at epoch: | 91.9888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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