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 01726U 26053.10110322 +.00000000 +00000-0 +13788-3 0 00005
2 01726 59.3791 287.7615 0718541 145.4774 7.8672 11.97074279 03
| Epoch (UTC): | 22 February 2026 02:25:35 |
| Eccentricity: | 0.0718541 |
| inclination: | 59.3791° |
| perigee height: | 1114 km |
| apogee height: | 2274 km |
| right ascension of ascending node: | 287.7615° |
| argument of perigee: | 145.4774° |
| revolutions per day: | 11.97074279 |
| mean anomaly at epoch: | 7.8672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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