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 04579U 26160.10296877 +.00000000 +00000-0 +90143-4 0 00004
2 04579 74.0024 290.2854 0010559 218.7221 141.3191 14.63692019 08
| Epoch (UTC): | 09 June 2026 02:28:16 |
| Eccentricity: | 0.0010559 |
| inclination: | 74.0024° |
| perigee height: | 674 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 290.2854° |
| argument of perigee: | 218.7221° |
| revolutions per day: | 14.63692019 |
| mean anomaly at epoch: | 141.3191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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