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 05118U 26159.44740534 +.00000000 +00000-0 +37548-3 0 00002
2 05118 81.2330 299.2734 0013675 312.7347 47.2758 15.68914098 03
| Epoch (UTC): | 08 June 2026 10:44:15 |
| Eccentricity: | 0.0013675 |
| inclination: | 81.2330° |
| perigee height: | 353 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 299.2734° |
| argument of perigee: | 312.7347° |
| revolutions per day: | 15.68914098 |
| mean anomaly at epoch: | 47.2758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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