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 43622U 26144.90976970 +.00000000 +00000-0 +00000-0 0 00004
2 43622 56.6058 63.4274 0008090 325.3050 34.6357 1.86231070 06
| Epoch (UTC): | 24 May 2026 21:50:04 |
| Eccentricity: | 0.0008090 |
| inclination: | 56.6058° |
| perigee height: | 21505 km |
| apogee height: | 21551 km |
| right ascension of ascending node: | 63.4274° |
| argument of perigee: | 325.3050° |
| revolutions per day: | 1.86231070 |
| mean anomaly at epoch: | 34.6357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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