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 55951U 26145.25622394 +.00000000 +00000-0 -13799-4 0 00003
2 55951 69.9998 91.2235 0003150 264.7636 95.3164 14.98335520 00
| Epoch (UTC): | 25 May 2026 06:08:57 |
| Eccentricity: | 0.0003150 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.2235° |
| argument of perigee: | 264.7636° |
| revolutions per day: | 14.98335520 |
| mean anomaly at epoch: | 95.3164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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