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 55644U 26145.55550112 +.00000000 +00000-0 -97275-5 0 00005
2 55644 69.9994 350.7125 0002568 268.9193 91.1672 14.98331319 02
| Epoch (UTC): | 25 May 2026 13:19:55 |
| Eccentricity: | 0.0002568 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 350.7125° |
| argument of perigee: | 268.9193° |
| revolutions per day: | 14.98331319 |
| mean anomaly at epoch: | 91.1672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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