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 17291U 26159.35303484 +.00000000 +00000-0 +24531-4 0 00005
2 17291 82.4671 107.7759 0010492 207.7084 152.3519 13.84691958 00
| Epoch (UTC): | 08 June 2026 08:28:22 |
| Eccentricity: | 0.0010492 |
| inclination: | 82.4671° |
| perigee height: | 940 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 107.7759° |
| argument of perigee: | 207.7084° |
| revolutions per day: | 13.84691958 |
| mean anomaly at epoch: | 152.3519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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