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 55314U 26145.34897147 +.00000000 +00000-0 +40581-4 0 00004
2 55314 69.9985 171.2257 0003363 269.2127 90.8647 14.98324764 07
| Epoch (UTC): | 25 May 2026 08:22:31 |
| Eccentricity: | 0.0003363 |
| inclination: | 69.9985° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 171.2257° |
| argument of perigee: | 269.2127° |
| revolutions per day: | 14.98324764 |
| mean anomaly at epoch: | 90.8647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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