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 19650U 26159.45849314 +.00000000 +00000-0 -16714-4 0 00009
2 19650 71.0004 320.5057 0016096 237.4780 122.4788 14.16166687 08
| Epoch (UTC): | 08 June 2026 11:00:13 |
| Eccentricity: | 0.0016096 |
| inclination: | 71.0004° |
| perigee height: | 827 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 320.5057° |
| argument of perigee: | 237.4780° |
| revolutions per day: | 14.16166687 |
| mean anomaly at epoch: | 122.4788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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