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 55780U 26145.10531763 +.00000000 +00000-0 +23208-4 0 00001
2 55780 69.9998 31.6186 0002872 270.0476 90.0354 14.98332465 03
| Epoch (UTC): | 25 May 2026 02:31:39 |
| Eccentricity: | 0.0002872 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.6186° |
| argument of perigee: | 270.0476° |
| revolutions per day: | 14.98332465 |
| mean anomaly at epoch: | 90.0354° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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