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 19468U 26162.60269501 +.00000000 +00000-0 +66501-5 0 00000
2 19468 98.9577 211.3505 0070365 307.1960 171.2020 14.03766052 06
| Epoch (UTC): | 11 June 2026 14:27:52 |
| Eccentricity: | 0.0070365 |
| inclination: | 98.9577° |
| perigee height: | 830 km |
| apogee height: | 932 km |
| right ascension of ascending node: | 211.3505° |
| argument of perigee: | 307.1960° |
| revolutions per day: | 14.03766052 |
| mean anomaly at epoch: | 171.2020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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