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 26140.76038993 +.00000000 +00000-0 +14524-4 0 00008
2 00016 34.2658 24.3679 2017771 4.6886 356.9870 10.49588214 05
| Epoch (UTC): | 20 May 2026 18:14:57 |
| Eccentricity: | 0.2017771 |
| inclination: | 34.2658° |
| perigee height: | 656 km |
| apogee height: | 4211 km |
| right ascension of ascending node: | 24.3679° |
| argument of perigee: | 4.6886° |
| revolutions per day: | 10.49588214 |
| mean anomaly at epoch: | 356.9870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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