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 26103.73579573 +.00000000 +00000-0 +10825-3 0 00007
2 00016 34.2641 131.3969 2019070 208.3952 139.0275 10.49583943 02
| Epoch (UTC): | 13 April 2026 17:39:32 |
| Eccentricity: | 0.2019070 |
| inclination: | 34.2641° |
| perigee height: | 654 km |
| apogee height: | 4213 km |
| right ascension of ascending node: | 131.3969° |
| argument of perigee: | 208.3952° |
| revolutions per day: | 10.49583943 |
| mean anomaly at epoch: | 139.0275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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