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 41622U 26053.08043226 +.00000000 +00000-0 +00000-0 0 00009
2 41622 2.4550 299.6388 0195786 262.9054 233.3463 1.00270267 01
| Epoch (UTC): | 22 February 2026 01:55:49 |
| Eccentricity: | 0.0195786 |
| inclination: | 2.4550° |
| perigee height: | 34961 km |
| apogee height: | 36613 km |
| right ascension of ascending node: | 299.6388° |
| argument of perigee: | 262.9054° |
| revolutions per day: | 1.00270267 |
| mean anomaly at epoch: | 233.3463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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