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 55399U 26145.63754740 +.00000000 +00000-0 +14750-4 0 00009
2 55399 69.9992 230.3517 0003495 270.7230 89.3528 14.98332090 04
| Epoch (UTC): | 25 May 2026 15:18:04 |
| Eccentricity: | 0.0003495 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.3517° |
| argument of perigee: | 270.7230° |
| revolutions per day: | 14.98332090 |
| mean anomaly at epoch: | 89.3528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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