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 26131.81111008 +.00000000 +00000-0 -12712-4 0 00001
2 00016 34.2708 50.2435 2018557 326.8954 21.9786 10.49588448 01
| Epoch (UTC): | 11 May 2026 19:27:59 |
| Eccentricity: | 0.2018557 |
| inclination: | 34.2708° |
| perigee height: | 655 km |
| apogee height: | 4212 km |
| right ascension of ascending node: | 50.2435° |
| argument of perigee: | 326.8954° |
| revolutions per day: | 10.49588448 |
| mean anomaly at epoch: | 21.9786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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