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 55651U 26145.55967767 +.00000000 +00000-0 -16347-3 0 00000
2 55651 69.9996 350.7268 0003177 269.8644 90.2151 14.98343574 06
| Epoch (UTC): | 25 May 2026 13:25:56 |
| Eccentricity: | 0.0003177 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 350.7268° |
| argument of perigee: | 269.8644° |
| revolutions per day: | 14.98343574 |
| mean anomaly at epoch: | 90.2151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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