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 26021.48524762 +.00000000 +00000-0 +21060-3 0 00009
2 04579 74.0000 196.8727 0009665 160.3557 199.7984 14.63517182 06
| Epoch (UTC): | 21 January 2026 11:38:45 |
| Eccentricity: | 0.0009665 |
| inclination: | 74.0000° |
| perigee height: | 675 km |
| apogee height: | 689 km |
| right ascension of ascending node: | 196.8727° |
| argument of perigee: | 160.3557° |
| revolutions per day: | 14.63517182 |
| mean anomaly at epoch: | 199.7984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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