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 55669U 26145.25901980 +.00000000 +00000-0 +51435-5 0 00009
2 55669 69.9996 331.4060 0002643 268.7961 91.2895 14.98329000 02
| Epoch (UTC): | 25 May 2026 06:12:59 |
| Eccentricity: | 0.0002643 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.4060° |
| argument of perigee: | 268.7961° |
| revolutions per day: | 14.98329000 |
| mean anomaly at epoch: | 91.2895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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