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 55784U 26145.66668980 +.00000000 +00000-0 -92399-3 0 00005
2 55784 70.0018 10.4517 0002473 268.1423 126.8738 14.98346905 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0002473 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.4517° |
| argument of perigee: | 268.1423° |
| revolutions per day: | 14.98346905 |
| mean anomaly at epoch: | 126.8738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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