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 26160.63998054 +.00000000 +00000-0 +21229-4 0 00008
2 17369 65.0117 268.5051 0017313 285.9264 73.9913 14.31872280 04
| Epoch (UTC): | 09 June 2026 15:21:34 |
| Eccentricity: | 0.0017313 |
| inclination: | 65.0117° |
| perigee height: | 773 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 268.5051° |
| argument of perigee: | 285.9264° |
| revolutions per day: | 14.31872280 |
| mean anomaly at epoch: | 73.9913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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