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 26159.13345580 +.00000000 +00000-0 +21454-3 0 00001
2 00016 34.2649 331.2473 2017009 82.2854 300.0661 10.49593259 01
| Epoch (UTC): | 08 June 2026 03:12:10 |
| Eccentricity: | 0.2017009 |
| inclination: | 34.2649° |
| perigee height: | 656 km |
| apogee height: | 4211 km |
| right ascension of ascending node: | 331.2473° |
| argument of perigee: | 82.2854° |
| revolutions per day: | 10.49593259 |
| mean anomaly at epoch: | 300.0661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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