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 17369U 26158.68436137 +.00000000 +00000-0 +30842-4 0 00000
2 17369 65.0119 273.9848 0017255 285.9801 73.9382 14.31872152 00
| Epoch (UTC): | 07 June 2026 16:25:28 |
| Eccentricity: | 0.0017255 |
| inclination: | 65.0119° |
| perigee height: | 773 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 273.9848° |
| argument of perigee: | 285.9801° |
| revolutions per day: | 14.31872152 |
| mean anomaly at epoch: | 73.9382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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