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 60604U 26145.17984479 +.00000000 +00000-0 -71275-4 0 00003
2 60604 53.1619 314.4828 0001241 99.6204 260.4937 15.30179897 02
| Epoch (UTC): | 25 May 2026 04:18:58 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.1619° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.4828° |
| argument of perigee: | 99.6204° |
| revolutions per day: | 15.30179897 |
| mean anomaly at epoch: | 260.4937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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