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 26158.75273251 +.00000000 +00000-0 +27061-3 0 00003
2 00016 34.2649 332.3478 2017017 80.6779 301.4897 10.49593348 00
| Epoch (UTC): | 07 June 2026 18:03:56 |
| Eccentricity: | 0.2017017 |
| inclination: | 34.2649° |
| perigee height: | 656 km |
| apogee height: | 4211 km |
| right ascension of ascending node: | 332.3478° |
| argument of perigee: | 80.6779° |
| revolutions per day: | 10.49593348 |
| mean anomaly at epoch: | 301.4897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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