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 55275U 26145.37854911 +.00000000 +00000-0 +73892-3 0 00005
2 55275 70.0007 191.2087 0003095 261.7357 98.3451 14.98362877 01
| Epoch (UTC): | 25 May 2026 09:05:06 |
| Eccentricity: | 0.0003095 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 191.2087° |
| argument of perigee: | 261.7357° |
| revolutions per day: | 14.98362877 |
| mean anomaly at epoch: | 98.3451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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