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 61539U 26145.48828088 +.00000000 +00000-0 +73567-5 0 00004
2 61539 53.1571 217.3863 0000918 80.2066 279.9055 15.69698552 01
| Epoch (UTC): | 25 May 2026 11:43:07 |
| Eccentricity: | 0.0000918 |
| inclination: | 53.1571° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 217.3863° |
| argument of perigee: | 80.2066° |
| revolutions per day: | 15.69698552 |
| mean anomaly at epoch: | 279.9055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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