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 55665U 26145.51772348 +.00000000 +00000-0 +57972-4 0 00009
2 55665 69.9994 330.7045 0002878 269.1559 90.9270 14.98334237 00
| Epoch (UTC): | 25 May 2026 12:25:31 |
| Eccentricity: | 0.0002878 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 330.7045° |
| argument of perigee: | 269.1559° |
| revolutions per day: | 14.98334237 |
| mean anomaly at epoch: | 90.9270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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