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 26088.10206169 +.00000000 +00000-0 -41330-4 0 00004
2 01726 59.3798 209.0702 0717230 168.3426 3.4359 11.97075417 05
| Epoch (UTC): | 29 March 2026 02:26:58 |
| Eccentricity: | 0.0717230 |
| inclination: | 59.3798° |
| perigee height: | 1115 km |
| apogee height: | 2273 km |
| right ascension of ascending node: | 209.0702° |
| argument of perigee: | 168.3426° |
| revolutions per day: | 11.97075417 |
| mean anomaly at epoch: | 3.4359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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