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 41590U 26045.02087419 +.00000000 +00000-0 +37328-3 0 00006
2 41590 23.7915 348.1393 7961025 263.3039 11.6171 1.45716373 09
| Epoch (UTC): | 14 February 2026 00:30:03 |
| Eccentricity: | 0.7961025 |
| inclination: | 23.7915° |
| perigee height: | 323 km |
| apogee height: | 52650 km |
| right ascension of ascending node: | 348.1393° |
| argument of perigee: | 263.3039° |
| revolutions per day: | 1.45716373 |
| mean anomaly at epoch: | 11.6171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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