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 26073.80188734 +.00000000 +00000-0 +62877-4 0 00007
2 00058 28.3266 258.6611 0164815 146.2644 214.8511 13.46426229 04
| Epoch (UTC): | 14 March 2026 19:14:43 |
| Eccentricity: | 0.0164815 |
| inclination: | 28.3266° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 258.6611° |
| argument of perigee: | 146.2644° |
| revolutions per day: | 13.46426229 |
| mean anomaly at epoch: | 214.8511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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