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 23482U 26063.45047889 +.00000000 +00000-0 -38073-1 0 00007
2 23482 64.7024 46.0247 0389774 207.5791 323.1620 11.31610351 05
| Epoch (UTC): | 04 March 2026 10:48:41 |
| Eccentricity: | 0.0389774 |
| inclination: | 64.7024° |
| perigee height: | 1676 km |
| apogee height: | 2329 km |
| right ascension of ascending node: | 46.0247° |
| argument of perigee: | 207.5791° |
| revolutions per day: | 11.31610351 |
| mean anomaly at epoch: | 323.1620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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