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 38709U 26145.56107859 +.00000000 +00000-0 +62388-4 0 00000
2 38709 98.9750 262.4434 0010049 233.1887 126.8370 14.24976846 06
| Epoch (UTC): | 25 May 2026 13:27:57 |
| Eccentricity: | 0.0010049 |
| inclination: | 98.9750° |
| perigee height: | 801 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 262.4434° |
| argument of perigee: | 233.1887° |
| revolutions per day: | 14.24976846 |
| mean anomaly at epoch: | 126.8370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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