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 55654U 26145.30515929 +.00000000 +00000-0 +19814-4 0 00007
2 55654 69.9999 351.4441 0002707 264.7504 95.3346 14.98330040 06
| Epoch (UTC): | 25 May 2026 07:19:25 |
| Eccentricity: | 0.0002707 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 351.4441° |
| argument of perigee: | 264.7504° |
| revolutions per day: | 14.98330040 |
| mean anomaly at epoch: | 95.3346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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