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 58622U 26145.27903369 +.00000000 +00000-0 +56801-5 0 00008
2 58622 43.0011 354.6537 0000821 271.2944 88.7814 15.27574336 06
| Epoch (UTC): | 25 May 2026 06:41:48 |
| Eccentricity: | 0.0000821 |
| inclination: | 43.0011° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.6537° |
| argument of perigee: | 271.2944° |
| revolutions per day: | 15.27574336 |
| mean anomaly at epoch: | 88.7814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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