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 26039.20886627 +.00000000 +00000-0 +40694-4 0 00006
2 00016 34.2795 318.0155 2022197 295.8636 44.7422 10.49576853 05
| Epoch (UTC): | 08 February 2026 05:00:46 |
| Eccentricity: | 0.2022197 |
| inclination: | 34.2795° |
| perigee height: | 652 km |
| apogee height: | 4215 km |
| right ascension of ascending node: | 318.0155° |
| argument of perigee: | 295.8636° |
| revolutions per day: | 10.49576853 |
| mean anomaly at epoch: | 44.7422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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