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 18958U 26044.72791331 +.00000000 +00000-0 +17370-3 0 00004
2 18958 82.5115 274.6204 0002741 297.6876 62.4079 15.17770658 04
| Epoch (UTC): | 13 February 2026 17:28:11 |
| Eccentricity: | 0.0002741 |
| inclination: | 82.5115° |
| perigee height: | 511 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 274.6204° |
| argument of perigee: | 297.6876° |
| revolutions per day: | 15.17770658 |
| mean anomaly at epoch: | 62.4079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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