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 22719U 26140.50991578 +.00000000 +00000-0 +00000-0 0 00001
2 22719 13.8845 14.3814 0001582 24.2554 322.7347 0.99049559 09
| Epoch (UTC): | 20 May 2026 12:14:16 |
| Eccentricity: | 0.0001582 |
| inclination: | 13.8845° |
| perigee height: | 36126 km |
| apogee height: | 36139 km |
| right ascension of ascending node: | 14.3814° |
| argument of perigee: | 24.2554° |
| revolutions per day: | 0.99049559 |
| mean anomaly at epoch: | 322.7347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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