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 08459U 26109.54270036 +.00000000 +00000-0 +21886-4 0 00003
2 08459 74.0596 303.7617 0015200 21.5421 338.6369 14.38223747 08
| Epoch (UTC): | 19 April 2026 13:01:29 |
| Eccentricity: | 0.0015200 |
| inclination: | 74.0596° |
| perigee height: | 754 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 303.7617° |
| argument of perigee: | 21.5421° |
| revolutions per day: | 14.38223747 |
| mean anomaly at epoch: | 338.6369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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