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 60438U 26145.50194816 +.00000000 +00000-0 +24977-4 0 00009
2 60438 53.1603 219.3409 0000882 69.1807 290.9290 15.34390049 07
| Epoch (UTC): | 25 May 2026 12:02:48 |
| Eccentricity: | 0.0000882 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.3409° |
| argument of perigee: | 69.1807° |
| revolutions per day: | 15.34390049 |
| mean anomaly at epoch: | 290.9290° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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