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 62889U 26145.53199303 +.00000000 +00000-0 +13991-2 0 00002
2 62889 43.0018 78.1089 0002312 273.7672 86.2932 15.70955988 03
| Epoch (UTC): | 25 May 2026 12:46:04 |
| Eccentricity: | 0.0002312 |
| inclination: | 43.0018° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 78.1089° |
| argument of perigee: | 273.7672° |
| revolutions per day: | 15.70955988 |
| mean anomaly at epoch: | 86.2932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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