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 27535U 26128.13830294 +.00000000 +00000-0 +73437-4 0 00002
2 27535 82.9329 340.0071 0037082 17.7505 100.1295 13.74694411 05
| Epoch (UTC): | 08 May 2026 03:19:09 |
| Eccentricity: | 0.0037082 |
| inclination: | 82.9329° |
| perigee height: | 955 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 340.0071° |
| argument of perigee: | 17.7505° |
| revolutions per day: | 13.74694411 |
| mean anomaly at epoch: | 100.1295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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