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 26161.13218272 +.00000000 +00000-0 +15595-3 0 00000
2 00016 34.2647 325.4698 2016970 90.7251 292.3282 10.49593622 00
| Epoch (UTC): | 10 June 2026 03:10:20 |
| Eccentricity: | 0.2016970 |
| inclination: | 34.2647° |
| perigee height: | 656 km |
| apogee height: | 4211 km |
| right ascension of ascending node: | 325.4698° |
| argument of perigee: | 90.7251° |
| revolutions per day: | 10.49593622 |
| mean anomaly at epoch: | 292.3282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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