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 17290U 26069.40345113 +.00000000 +00000-0 +57342-4 0 00001
2 17290 82.4708 175.3356 0014288 91.8034 268.4763 13.85262087 06
| Epoch (UTC): | 10 March 2026 09:40:58 |
| Eccentricity: | 0.0014288 |
| inclination: | 82.4708° |
| perigee height: | 935 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 175.3356° |
| argument of perigee: | 91.8034° |
| revolutions per day: | 13.85262087 |
| mean anomaly at epoch: | 268.4763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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