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 00011U 26149.42873350 +.00000000 +00000-0 +76759-3 0 00006
2 00011 32.8709 156.1572 1445232 310.1200 38.1220 11.90453572 01
| Epoch (UTC): | 29 May 2026 10:17:22 |
| Eccentricity: | 0.1445232 |
| inclination: | 32.8709° |
| perigee height: | 553 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 156.1572° |
| argument of perigee: | 310.1200° |
| revolutions per day: | 11.90453572 |
| mean anomaly at epoch: | 38.1220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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