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 39773U 26145.58424844 +.00000000 +00000-0 +00000-0 0 00009
2 39773 0.0689 17.0755 0004049 44.4967 35.0266 1.00273371 06
| Epoch (UTC): | 25 May 2026 14:01:19 |
| Eccentricity: | 0.0004049 |
| inclination: | 0.0689° |
| perigee height: | 35769 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 17.0755° |
| argument of perigee: | 44.4967° |
| revolutions per day: | 1.00273371 |
| mean anomaly at epoch: | 35.0266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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