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 18550U 26088.07042275 +.00000000 +00000-0 +84408-4 0 00001
2 18550 71.0256 326.3443 0182070 193.9435 165.6606 13.79260958 09
| Epoch (UTC): | 29 March 2026 01:41:24 |
| Eccentricity: | 0.0182070 |
| inclination: | 71.0256° |
| perigee height: | 833 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 326.3443° |
| argument of perigee: | 193.9435° |
| revolutions per day: | 13.79260958 |
| mean anomaly at epoch: | 165.6606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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