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 55421U 26145.53764639 +.00000000 +00000-0 +43998-4 0 00008
2 55421 69.9995 250.6757 0003051 267.0687 93.0123 14.98329341 05
| Epoch (UTC): | 25 May 2026 12:54:12 |
| Eccentricity: | 0.0003051 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.6757° |
| argument of perigee: | 267.0687° |
| revolutions per day: | 14.98329341 |
| mean anomaly at epoch: | 93.0123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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