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 55779U 26145.61413029 +.00000000 +00000-0 +85891-5 0 00006
2 55779 70.0007 10.3021 0002644 270.0389 90.0467 14.98328590 06
| Epoch (UTC): | 25 May 2026 14:44:20 |
| Eccentricity: | 0.0002644 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 10.3021° |
| argument of perigee: | 270.0389° |
| revolutions per day: | 14.98328590 |
| mean anomaly at epoch: | 90.0467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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