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,
| Epoch (UTC): | 15 January 2026 12:13:53 |
| Eccentricity: | 0.1839551 |
| inclination: | 34.2470° |
| perigee height: | 651 km |
| apogee height: | 3820 km |
| right ascension of ascending node: | 65.4923° |
| argument of perigee: | 170.1011° |
| revolutions per day: | 10.85940602 |
| mean anomaly at epoch: | 194.1623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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