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 55435U 26145.62549793 +.00000000 +00000-0 +93077-4 0 00008
2 55435 69.9993 270.4407 0002837 278.1125 81.9712 14.98336871 07
| Epoch (UTC): | 25 May 2026 15:00:43 |
| Eccentricity: | 0.0002837 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.4407° |
| argument of perigee: | 278.1125° |
| revolutions per day: | 14.98336871 |
| mean anomaly at epoch: | 81.9712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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