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 19223U 26106.16721359 +.00000000 +00000-0 +71408-4 0 00003
2 19223 89.9821 78.0502 0031584 33.7042 337.8539 13.22952354 02
| Epoch (UTC): | 16 April 2026 04:00:47 |
| Eccentricity: | 0.0031584 |
| inclination: | 89.9821° |
| perigee height: | 1150 km |
| apogee height: | 1197 km |
| right ascension of ascending node: | 78.0502° |
| argument of perigee: | 33.7042° |
| revolutions per day: | 13.22952354 |
| mean anomaly at epoch: | 337.8539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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