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 61588U 26145.50034046 +.00000000 +00000-0 +31304-4 0 00006
2 61588 53.1604 67.5507 0001165 101.8454 258.2680 15.34385710 03
| Epoch (UTC): | 25 May 2026 12:00:29 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 67.5507° |
| argument of perigee: | 101.8454° |
| revolutions per day: | 15.34385710 |
| mean anomaly at epoch: | 258.2680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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