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 62891U 26145.50558243 +.00000000 +00000-0 +17043-2 0 00006
2 62891 43.0001 78.7993 0000692 345.6038 14.4809 15.70901692 01
| Epoch (UTC): | 25 May 2026 12:08:02 |
| Eccentricity: | 0.0000692 |
| inclination: | 43.0001° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 78.7993° |
| argument of perigee: | 345.6038° |
| revolutions per day: | 15.70901692 |
| mean anomaly at epoch: | 14.4809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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