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 26159.48783191 +.00000000 +00000-0 +10545-3 0 00000
2 04579 74.0024 291.4686 0010578 219.9097 140.1294 14.63691707 03
| Epoch (UTC): | 08 June 2026 11:42:28 |
| Eccentricity: | 0.0010578 |
| inclination: | 74.0024° |
| perigee height: | 674 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 291.4686° |
| argument of perigee: | 219.9097° |
| revolutions per day: | 14.63691707 |
| mean anomaly at epoch: | 140.1294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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