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 26605U 26145.16629066 +.00000000 +00000-0 +00000-0 0 00006
2 26605 55.6137 95.8632 0174381 266.5986 239.4730 2.00566589 06
| Epoch (UTC): | 25 May 2026 03:59:27 |
| Eccentricity: | 0.0174381 |
| inclination: | 55.6137° |
| perigee height: | 19719 km |
| apogee height: | 20645 km |
| right ascension of ascending node: | 95.8632° |
| argument of perigee: | 266.5986° |
| revolutions per day: | 2.00566589 |
| mean anomaly at epoch: | 239.4730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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