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 39481U 26145.56648169 +.00000000 +00000-0 +00000-0 0 00001
2 39481 0.0387 103.1717 0002660 306.0889 310.6274 1.00272680 02
| Epoch (UTC): | 25 May 2026 13:35:44 |
| Eccentricity: | 0.0002660 |
| inclination: | 0.0387° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 103.1717° |
| argument of perigee: | 306.0889° |
| revolutions per day: | 1.00272680 |
| mean anomaly at epoch: | 310.6274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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