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 18957U 26076.17980773 +.00000000 +00000-0 +77834-5 0 00000
2 18957 65.0468 9.9278 0060572 266.0043 93.4089 13.79813828 00
| Epoch (UTC): | 17 March 2026 04:18:55 |
| Eccentricity: | 0.0060572 |
| inclination: | 65.0468° |
| perigee height: | 920 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 9.9278° |
| argument of perigee: | 266.0043° |
| revolutions per day: | 13.79813828 |
| mean anomaly at epoch: | 93.4089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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