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 00058U 26037.17433914 +.00000000 +00000-0 +56645-4 0 00006
2 00058 28.3280 84.5090 0164753 202.9155 156.3969 13.46424093 09
| Epoch (UTC): | 06 February 2026 04:11:02 |
| Eccentricity: | 0.0164753 |
| inclination: | 28.3280° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 84.5090° |
| argument of perigee: | 202.9155° |
| revolutions per day: | 13.46424093 |
| mean anomaly at epoch: | 156.3969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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