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 55429U 26145.55851744 +.00000000 +00000-0 -72578-4 0 00009
2 55429 69.9992 250.7498 0003039 267.0048 93.0763 14.98336767 00
| Epoch (UTC): | 25 May 2026 13:24:15 |
| Eccentricity: | 0.0003039 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 250.7498° |
| argument of perigee: | 267.0048° |
| revolutions per day: | 14.98336767 |
| mean anomaly at epoch: | 93.0763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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