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 55742U 26145.17650396 +.00000000 +00000-0 +20175-4 0 00000
2 55742 70.0009 51.7490 0002181 279.2774 80.8138 14.98332049 08
| Epoch (UTC): | 25 May 2026 04:14:09 |
| Eccentricity: | 0.0002181 |
| inclination: | 70.0009° |
| perigee height: | 571 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.7490° |
| argument of perigee: | 279.2774° |
| revolutions per day: | 14.98332049 |
| mean anomaly at epoch: | 80.8138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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