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 17304U 26040.52322766 +.00000000 +00000-0 +11822-3 0 00000
2 17304 74.0568 39.9478 0028788 170.2672 189.9047 14.39127546 05
| Epoch (UTC): | 09 February 2026 12:33:26 |
| Eccentricity: | 0.0028788 |
| inclination: | 74.0568° |
| perigee height: | 741 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 39.9478° |
| argument of perigee: | 170.2672° |
| revolutions per day: | 14.39127546 |
| mean anomaly at epoch: | 189.9047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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