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 00016U 26129.81188477 +.00000000 +00000-0 +11770-4 0 00004
2 00016 34.2721 56.0226 2018730 318.4554 27.8685 10.49588549 09
| Epoch (UTC): | 09 May 2026 19:29:06 |
| Eccentricity: | 0.2018730 |
| inclination: | 34.2721° |
| perigee height: | 655 km |
| apogee height: | 4212 km |
| right ascension of ascending node: | 56.0226° |
| argument of perigee: | 318.4554° |
| revolutions per day: | 10.49588549 |
| mean anomaly at epoch: | 27.8685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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